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GRUS-1A

In orbit NORAD 43890 YYIR-8416-3126-1290-3889 Russia

2018

Launch

0

Observations all time

Mission information
Spacecraft name
GRUS-1A
Other names
2018-111Q
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
2018-12-27 00:00:00
Separation time
2018-12-27 00:00:00
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
561.52 km
Apogee
573.04 km
Inclination
97.4°
Period
96.1 min
Semi-major axis
6945.4 km
Velocity
7.57 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 20:56:55 UTC
Two-line elements (TLE)
1 43890U 18111Q   26283.59838278 -.00000048  00000-0  63146-6 0  9996
2 43890 97.4331 145.4978 0008311 118.9349 241.2709 14.98903059424990
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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 07:30:01 GRUS-1A
NORAD 43890
STARLINK-5469
NORAD 55649
4.996 14.51 2.3e-06
2026-10-13 07:16:00 GRUS-1A
NORAD 43890
STARLINK-35715
NORAD 66841
4.477 3.60 6.5e-06
2026-10-13 08:52:16 GRUS-1A
NORAD 43890
STARLINK-35715
NORAD 66841
1.994 3.60 3.3e-05
2026-10-13 10:28:31 GRUS-1A
NORAD 43890
STARLINK-35715
NORAD 66841
3.708 3.61 9.5e-06
2026-10-13 14:00:33 GRUS-1A
NORAD 43890
NOAA 16 DEB
NORAD 41094
4.801 11.71 1.3e-07
2026-10-13 14:54:10 GRUS-1A
NORAD 43890
ICEYE-X57
NORAD 64578
1.545 11.90 1.2e-06
2026-10-13 18:40:58 GRUS-1A
NORAD 43890
STARLINK-36182
NORAD 67192
3.978 14.90 3.1e-06
2026-10-13 20:54:17 GRUS-1A
NORAD 43890
STARLINK-35715
NORAD 66841
3.829 3.63 8.9e-06
2026-10-13 21:45:09 GRUS-1A
NORAD 43890
STRIX-5
NORAD 65971
4.553 14.03 1.0e-07
2026-10-13 22:30:33 GRUS-1A
NORAD 43890
STARLINK-35715
NORAD 66841
0.856 3.63 1.8e-04
2026-10-13 22:54:07 GRUS-1A
NORAD 43890
PEGASUS DEB
NORAD 24817
4.142 11.62 1.8e-07
2026-10-13 23:18:33 GRUS-1A
NORAD 43890
STARLINK-35476
NORAD 66825
1.790 3.63 4.1e-05
2026-10-14 00:06:48 GRUS-1A
NORAD 43890
STARLINK-35715
NORAD 66841
3.227 3.64 1.2e-05
2026-10-14 00:54:49 GRUS-1A
NORAD 43890
STARLINK-35476
NORAD 66825
4.689 3.64 5.9e-06
2026-10-14 08:08:04 GRUS-1A
NORAD 43890
STARLINK-35476
NORAD 66825
2.670 3.66 1.8e-05
2026-10-14 09:44:19 GRUS-1A
NORAD 43890
STARLINK-35476
NORAD 66825
3.252 3.67 1.2e-05
2026-10-14 12:35:33 GRUS-1A
NORAD 43890
ICEYE-X39
NORAD 60546
4.726 14.34 8.8e-08
2026-10-15 05:59:19 PROBA-1
NORAD 26958
GRUS-1A
NORAD 43890
4.595 14.49 5.6e-08
2026-10-15 13:14:01 GRUS-1A
NORAD 43890
STARLINK-3072
NORAD 49153
3.554 10.97 7.7e-06
2026-10-15 20:33:58 GRUS-1A
NORAD 43890
BRO-12
NORAD 59108
4.991 10.59 1.3e-07
2026-10-16 07:28:15 GRUS-1A
NORAD 43890
STARLINK-36280
NORAD 67211
4.394 15.02 2.4e-06
2026-10-16 08:16:21 GRUS-1A
NORAD 43890
STARLINK-36280
NORAD 67211
3.950 15.04 3.0e-06
2026-10-16 09:04:15 GRUS-1A
NORAD 43890
STARLINK-36270
NORAD 67200
4.895 15.02 2.0e-06
2026-10-16 09:17:55 GRUS-1A
NORAD 43890
PEGASUS DEB
NORAD 39919
4.974 15.20 6.0e-08
2026-10-17 00:04:22 GRUS-1A
NORAD 43890
STARLINK-5467
NORAD 55660
3.836 15.03 3.2e-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