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KINEIS-5E

In orbit NORAD 62083 DJTQ-0143-2398-3239-9294

2024

Launch

12

Observations all time

Mission information
Spacecraft name
KINEIS-5E
Other names
2024-219C
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
2024-11-25 00:00:00
Separation time
2024-11-25 00:00:00
Last observers
Observer
Time of receipt
2026-08-03 15:08:47 UTC
2026-08-03 01:47:08 UTC
2026-08-03 00:14:56 UTC
2026-05-31 16:28:24 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
647.13 km
Apogee
654.36 km
Inclination
97.9°
Period
97.8 min
Semi-major axis
7028.9 km
Velocity
7.53 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-12 13:08:40 UTC
Two-line elements (TLE)
1 62083U 24219C   26285.33865000  .00000631  00000-0  10749-3 0  9999
2 62083 97.9133 81.0856 0005178 245.8255 114.2412 14.72313688101003
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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
2026-10-13 05:53:13 KINEIS-5E
NORAD 62083
COSMOS 2251 DEB
NORAD 34007
3.332 5.69 3.7e-07
2026-10-13 20:20:14 KINEIS-5E
NORAD 62083
FENGYUN 1C DEB
NORAD 35153
4.397 13.54 1.2e-07
2026-10-14 12:49:32 KINEIS-5E
NORAD 62083
COSMOS 2251 DEB
NORAD 34323
2.601 14.69 2.6e-07
2026-10-15 01:59:12 KINEIS-5E
NORAD 62083
OPS 8180 (STP RADSAT)
NORAD 6217
3.361 14.77 1.5e-07
2026-10-15 08:13:07 KINEIS-5E
NORAD 62083
CZ-6A DEB
NORAD 61308
0.930 14.83 1.9e-06
2026-10-15 12:08:46 KINEIS-5E
NORAD 62083
COSMOS 2251 DEB
NORAD 40808
3.214 14.99 1.5e-07
2026-10-15 13:59:41 KINEIS-5E
NORAD 62083
IRIDIUM 33 DEB
NORAD 34926
2.528 14.15 3.2e-07
2026-10-16 03:27:07 KINEIS-5E
NORAD 62083
YAOGAN-11 DEB
NORAD 38174
4.273 14.96 8.6e-08
2026-10-17 03:35:24 KINEIS-5E
NORAD 62083
COSMOS 2251 DEB
NORAD 34274
4.718 12.20 1.3e-07
2026-10-18 06:30:05 KINEIS-5E
NORAD 62083
COSMOS 2251 DEB
NORAD 40235
2.661 12.95 3.6e-07
2026-10-18 13:01:41 KINEIS-5E
NORAD 62083
PEGASUS DEB
NORAD 39308
4.472 15.12 7.4e-08

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