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2026-027C

In orbit NORAD 67748 DKAP-4218-9730-2522-6587 China

2026

Launch

0

Observations all time

Mission information
Spacecraft name
2026-027C
Other names
2027-027C
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Launch time
2026-02-12 00:00:00
Separation time
2026-02-12 00:00:00
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
496.45 km
Apogee
511.11 km
Inclination
97.5°
Period
94.8 min
Semi-major axis
6881.9 km
Velocity
7.6 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 20:56:59 UTC
Two-line elements (TLE)
1 67748U 26027C   26283.60433256  .00004307  00000-0  20480-3 0  9990
2 67748 97.5225 51.1793 0010714 170.3477 189.7965 15.19684129 36484
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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
2026-10-11 00:39:24 YAOGAN-43 02E
NORAD 60949
OBJECT C
NORAD 67748
4.989 13.33 1.0e-07
2026-10-11 04:20:00 ION SCV-020
NORAD 64545
OBJECT C
NORAD 67748
4.598 1.83 2.1e-07
2026-10-11 05:54:49 ION SCV-020
NORAD 64545
OBJECT C
NORAD 67748
4.334 1.83 2.3e-07
2026-10-11 12:13:23 OBJECT C
NORAD 67748
RASSVET-3 1
NORAD 68360
2.980 14.93 1.9e-07
2026-10-11 13:00:51 OBJECT C
NORAD 67748
RASSVET-3 1
NORAD 68360
4.496 14.96 8.2e-08
2026-10-11 17:13:47 OBJECT C
NORAD 67748
T.MICROSAT-2
NORAD 68433
1.909 15.01 4.4e-07
2026-10-12 06:28:03 HJ-2E
NORAD 54035
OBJECT C
NORAD 67748
3.608 13.41 1.9e-07
2026-10-12 07:59:57 BUGSAT-1 (TITA)
NORAD 40014
OBJECT C
NORAD 67748
1.936 3.66 1.1e-06
2026-10-12 23:08:56 STARLINK-5862
NORAD 55920
OBJECT C
NORAD 67748
4.187 6.38 7.0e-06
2026-10-13 23:44:25 OBJECT C
NORAD 67748
TRANSPORTER-16 OBJECT L
NORAD 68426
2.102 15.05 3.6e-07
2026-10-14 05:00:51 OBJECT C
NORAD 67748
RASSVET-3 9
NORAD 68368
4.734 15.04 7.1e-08
2026-10-14 06:35:43 OBJECT C
NORAD 67748
RASSVET-3 9
NORAD 68368
0.158 15.04 6.4e-05
2026-10-14 08:10:34 OBJECT C
NORAD 67748
RASSVET-3 9
NORAD 68368
4.606 15.04 7.4e-08
2026-10-15 14:56:02 OBJECT C
NORAD 67748
EYCORE-1
NORAD 69011
3.716 13.58 1.7e-07
2026-10-15 16:49:40 OBJECT C
NORAD 67748
JACK-002
NORAD 68417
4.587 15.05 7.6e-08
2026-10-15 17:29:33 LEMUR-2-NEUROSPICY
NORAD 63355
OBJECT C
NORAD 67748
2.303 14.62 3.5e-07
2026-10-16 03:39:22 CO3D 2
NORAD 64902
OBJECT C
NORAD 67748
3.324 6.46 3.7e-07
2026-10-16 08:23:54 PIAST-M
NORAD 66758
OBJECT C
NORAD 67748
3.806 7.07 2.7e-07
2026-10-16 10:12:52 OBJECT C
NORAD 67748
IRIDE-MS1-EAGLET 2-10
NORAD 68451
4.162 15.05 9.3e-08
2026-10-16 11:47:40 OBJECT C
NORAD 67748
IRIDE-MS1-EAGLET 2-10
NORAD 68451
4.292 15.05 8.7e-08
2026-10-16 15:18:15 YUNYAO-1 19
NORAD 58759
OBJECT C
NORAD 67748
0.782 13.22 4.1e-06
2026-10-16 19:27:30 CO3D 1
NORAD 64903
OBJECT C
NORAD 67748
2.060 6.47 9.5e-07
2026-10-16 21:49:40 CO3D 1
NORAD 64903
OBJECT C
NORAD 67748
4.910 6.45 1.7e-07

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