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KINEIS-1B

In orbit NORAD 60079 FGNF-7996-2438-8741-1021 France

Time in UTC

12.10 15:25

Scheduled · Два тюленя

78

Observations over 30 days

86%

Successful observations

186

Frames, latest 2026-10-07 06:02 UTC

Mission information
Spacecraft name
KINEIS-1B
Status
Active
The satellite is in orbit
Launch and timeline
Launch time
2024-06-20 00:00:00
Separation time
Last observers
Observer
Time of receipt
2026-10-07 06:02:29 UTC
2026-10-05 08:37:41 UTC
2026-10-05 06:55:47 UTC
2026-10-02 06:04:11 UTC
2026-10-01 05:40:02 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
621.24 km
Apogee
626.61 km
Inclination
98.0°
Period
97.2 min
Semi-major axis
7002.1 km
Velocity
7.55 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-12 05:08:35 UTC
Two-line elements (TLE)
1 60079U 24114A   26284.95931153  .00000899  00000-0  12357-3 0  9999
2 60079 97.9780 308.5731 0003830 84.1291 276.0357 14.80774911124683
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Orbit history, past year

Mean elements of every TLE set over the past 365 days, plotted against the epoch of the set. Each source is its own line; click it in the legend to hide it. A jump in altitude is a manoeuvre or a bad set; lines drifting apart are a disagreement between sources. “TLE age” is how many hours have passed since the epoch of the source's freshest set, plotted against when the set reached us, on a logarithmic scale. A set the source repeats unchanged does not reset the age.

Prediction divergence

Each TLE set is propagated with SGP4 to the epoch of the next set from the same source and compared with it, plotted against the epoch of the next set; the tooltip shows how many hours ahead the prediction ran. The logarithmic scale shows the size of the divergence and the tooltip its sign: plus along-track means the prediction is ahead of the satellite. This is how well the sets agree, not the true error: the reference is a TLE too, off by about a kilometre. An outlier is a manoeuvre between sets. Sets more than a week apart are not compared.

Time of closest approach, UTC Object 1 Object 2 Distance, km Speed, km/s Max. probability
2026-10-12 09:45:23 KINEIS-1B
NORAD 60079
KUIPER-00167
NORAD 65780
4.741 13.89 9.7e-08
2026-10-12 09:48:02 KINEIS-1B
NORAD 60079
KUIPER-00423
NORAD 69592
1.500 11.88 1.3e-06
2026-10-12 10:34:03 KINEIS-1B
NORAD 60079
KUIPER-00167
NORAD 65780
3.956 13.92 1.4e-07
2026-10-12 11:25:20 KINEIS-1B
NORAD 60079
KUIPER-00423
NORAD 69592
1.447 11.90 1.4e-06
2026-10-12 13:02:38 KINEIS-1B
NORAD 60079
KUIPER-00423
NORAD 69592
1.356 11.93 1.6e-06
2026-10-12 14:39:56 KINEIS-1B
NORAD 60079
KUIPER-00423
NORAD 69592
1.280 11.95 1.8e-06
2026-10-12 16:17:15 KINEIS-1B
NORAD 60079
KUIPER-00423
NORAD 69592
1.311 11.97 1.7e-06
2026-10-12 17:54:33 KINEIS-1B
NORAD 60079
KUIPER-00423
NORAD 69592
1.546 11.99 1.2e-06
2026-10-12 19:31:51 KINEIS-1B
NORAD 60079
KUIPER-00423
NORAD 69592
2.009 12.02 7.2e-07
2026-10-12 21:09:09 KINEIS-1B
NORAD 60079
KUIPER-00423
NORAD 69592
2.668 12.04 4.1e-07
2026-10-12 22:46:28 KINEIS-1B
NORAD 60079
KUIPER-00423
NORAD 69592
3.490 12.06 2.4e-07
2026-10-13 00:23:46 KINEIS-1B
NORAD 60079
KUIPER-00423
NORAD 69592
4.454 12.09 1.5e-07
2026-10-13 00:54:43 KINEIS-1B
NORAD 60079
KUIPER-00274
NORAD 67792
2.607 6.07 6.0e-07
2026-10-13 07:41:39 KINEIS-1B
NORAD 60079
KUIPER-00423
NORAD 69592
4.698 12.21 1.3e-07
2026-10-13 09:18:57 KINEIS-1B
NORAD 60079
KUIPER-00423
NORAD 69592
3.305 12.23 2.6e-07
2026-10-13 10:44:22 KINEIS-1B
NORAD 60079
FENGYUN 1C DEB
NORAD 36657
4.327 14.94 8.6e-08
2026-10-13 10:56:15 KINEIS-1B
NORAD 60079
KUIPER-00423
NORAD 69592
2.263 12.26 5.5e-07
2026-10-13 10:57:00 KINEIS-1B
NORAD 60079
UNKNOWN
NORAD 81845
2.776 14.67 2.3e-07
2026-10-13 12:33:33 KINEIS-1B
NORAD 60079
KUIPER-00423
NORAD 69592
2.428 12.28 4.8e-07
2026-10-13 13:24:21 KINEIS-1B
NORAD 60079
CP8 (IPEX)
NORAD 39471
3.888 9.25 2.4e-07
2026-10-13 14:02:30 KINEIS-1B
NORAD 60079
KUIPER-00111
NORAD 65149
4.048 6.37 2.5e-07
2026-10-13 14:10:52 KINEIS-1B
NORAD 60079
KUIPER-00423
NORAD 69592
3.816 12.30 1.9e-07
2026-10-13 16:28:30 KINEIS-1B
NORAD 60079
KUIPER-00111
NORAD 65149
4.229 6.39 2.3e-07
2026-10-13 21:59:14 KINEIS-1B
NORAD 60079
KUIPER-00641
NORAD 69787
4.305 14.52 1.0e-07
2026-10-14 03:47:25 KINEIS-1B
NORAD 60079
KUIPER-00153
NORAD 65773
3.680 14.53 1.4e-07
2026-10-14 04:36:05 KINEIS-1B
NORAD 60079
KUIPER-00153
NORAD 65773
2.944 14.54 2.1e-07
2026-10-14 20:57:36 KINEIS-1B
NORAD 60079
KUIPER-00431
NORAD 68936
3.772 8.72 2.6e-07
2026-10-14 21:46:14 KINEIS-1B
NORAD 60079
KUIPER-00431
NORAD 68936
4.817 8.72 1.6e-07
2026-10-15 06:38:22 KINEIS-1B
NORAD 60079
KUIPER-00188
NORAD 67142
2.891 14.28 2.4e-07
2026-10-15 09:18:08 KINEIS-1B
NORAD 60079
UNKNOWN
NORAD 270444
4.131 7.78 2.3e-07
2026-10-15 12:34:43 LINGQIAO VIDEO B
NORAD 40960
KINEIS-1B
NORAD 60079
2.514 4.30 6.7e-07
2026-10-15 23:19:01 KINEIS-1B
NORAD 60079
KUIPER-00140
NORAD 65965
3.725 13.81 1.6e-07
2026-10-16 18:22:11 KINEIS-1B
NORAD 60079
KUIPER-00210
NORAD 67146
2.646 13.77 3.2e-07
2026-10-17 03:04:11 KINEIS-1B
NORAD 60079
KUIPER-00152
NORAD 65772
0.670 14.57 4.1e-06
2026-10-17 03:52:51 KINEIS-1B
NORAD 60079
KUIPER-00152
NORAD 65772
1.071 14.57 1.6e-06
2026-10-17 04:07:50 KINEIS-1B
NORAD 60079
KUIPER-00440
NORAD 68942
2.469 10.77 5.4e-07
2026-10-17 04:49:10 KINEIS-1B
NORAD 60079
KUIPER-00150
NORAD 65770
2.523 14.42 3.0e-07
2026-10-17 05:37:50 KINEIS-1B
NORAD 60079
KUIPER-00150
NORAD 65770
4.567 14.44 9.1e-08
2026-10-17 05:45:09 KINEIS-1B
NORAD 60079
KUIPER-00440
NORAD 68942
3.715 10.80 2.4e-07
2026-10-17 08:11:05 KINEIS-1B
NORAD 60079
KUIPER-00440
NORAD 68942
3.674 10.81 2.4e-07
2026-10-17 09:48:24 KINEIS-1B
NORAD 60079
KUIPER-00440
NORAD 68942
1.399 10.84 1.7e-06
2026-10-17 11:25:42 KINEIS-1B
NORAD 60079
KUIPER-00440
NORAD 68942
4.684 10.86 1.5e-07
2026-10-17 21:06:49 KINEIS-1B
NORAD 60079
KUIPER-00547
NORAD 69615
3.668 13.94 1.6e-07
2026-10-18 00:45:30 KINEIS-1B
NORAD 60079
KUIPER-00092
NORAD 64837
2.069 9.85 8.1e-07
2026-10-18 04:48:45 KINEIS-1B
NORAD 60079
KUIPER-00092
NORAD 64837
1.441 9.80 1.7e-06

Data: CelesTrak SOCRATES Plus, computed from TLEs of the public catalog. This is an estimate, not grounds for a manoeuvre: TLEs carry no covariance, and the maximum probability assumes a position error.

All conjunctions of this satellite