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GRUS-3C

In orbit NORAD 69891 LWCK-6249-6810-8417-1354

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
GRUS-3C
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
585.67 km
Apogee
593.98 km
Inclination
97.7°
Period
96.5 min
Semi-major axis
6968.0 km
Velocity
7.55 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 04:46:21 UTC
Two-line elements (TLE)
1 69891U 26156Y   26282.46146839  .00000797  00000-0  84834-4 0  9998
2 69891 97.7410 181.2658 0005962 176.9905 183.1351 14.91645076 14036
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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 13:22:39 GRUS-3C
NORAD 69891
LEMUR-2-DELOITTE-4
NORAD 69934
4.352 0.03 2.3e-07
2026-10-11 14:08:38 RCM-3
NORAD 44323
GRUS-3C
NORAD 69891
3.778 12.03 2.0e-07
2026-10-11 15:55:00 GRUS-3C
NORAD 69891
SL-12 DEB
NORAD 23292
4.895 11.43 1.4e-07
2026-10-12 17:53:56 GRUS-3C
NORAD 69891
CZ-6A DEB
NORAD 54927
1.602 14.96 6.2e-07
2026-10-12 21:49:30 GRUS-3C
NORAD 69891
CZ-6A DEB
NORAD 55532
3.394 14.89 1.4e-07
2026-10-13 07:44:07 FFLY02
NORAD 65322
GRUS-3C
NORAD 69891
4.075 14.96 9.6e-08
2026-10-13 09:20:40 FFLY02
NORAD 65322
GRUS-3C
NORAD 69891
3.779 14.96 1.1e-07
2026-10-14 10:33:29 GRUS-3C
NORAD 69891
FENGYUN 1C DEB
NORAD 29872
3.575 12.66 2.1e-07
2026-10-14 13:49:29 SPIRONE
NORAD 66657
GRUS-3C
NORAD 69891
3.393 3.74 3.7e-07
2026-10-15 15:18:36 GRUS-3C
NORAD 69891
CZ-6A DEB
NORAD 55902
3.828 14.94 1.1e-07
2026-10-16 05:36:34 GRUS-3C
NORAD 69891
OBJECT J
NORAD 44887
4.819 14.96 6.8e-08
2026-10-16 07:13:08 GRUS-3C
NORAD 69891
OBJECT J
NORAD 44887
2.316 14.96 2.9e-07
2026-10-16 08:49:42 GRUS-3C
NORAD 69891
OBJECT J
NORAD 44887
3.643 14.96 1.2e-07
2026-10-16 09:21:46 GRUS-3C
NORAD 69891
FENGYUN 1C DEB
NORAD 37595
1.788 0.75 1.4e-06
2026-10-16 18:09:15 GRUS-3C
NORAD 69891
OASIS ALPHA
NORAD 69936
4.817 0.02 1.9e-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