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GRUS-1B

In orbit NORAD 47934 PLUI-2175-9332-5699-1162 Japan

2021

Launch

3

Observations all time

Mission information
Spacecraft name
GRUS-1B
Other names
2021-022C
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
2021-03-22 00:00:00
Separation time
2021-03-22 00:00:00
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
557.44 km
Apogee
577.02 km
Inclination
97.5°
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 12:56:47 UTC
Two-line elements (TLE)
1 47934U 21022C   26283.27128066  .00000788  00000-0  69818-4 0  9996
2 47934 97.5170 162.5391 0014096 290.6122 69.3589 14.98921231303137
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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
2026-10-10 20:34:04 GRUS-1B
NORAD 47934
FENGYUN 1C DEB
NORAD 30960
4.254 10.34 1.9e-07
2026-10-11 00:16:34 GRUS-1B
NORAD 47934
STARLINK-36182
NORAD 67192
2.050 15.02 1.1e-05
2026-10-11 03:57:54 GRUS-1B
NORAD 47934
ION SCV-012
NORAD 60573
4.700 14.92 7.4e-08
2026-10-11 09:37:58 GRUS-1B
NORAD 47934
OBJECT L
NORAD 61904
1.703 14.98 5.5e-07
2026-10-11 16:52:40 GRUS-1B
NORAD 47934
STARLINK-5456
NORAD 55667
4.849 15.05 2.0e-06
2026-10-11 21:58:37 GRUS-1B
NORAD 47934
STARLINK-5469
NORAD 55649
4.819 14.92 2.1e-06
2026-10-11 22:19:22 GRUS-1B
NORAD 47934
OBJECT C
NORAD 69099
2.088 14.77 4.0e-07
2026-10-11 22:58:40 GRUS-1B
NORAD 47934
COSMOS 2583
NORAD 62904
4.970 14.67 7.3e-08
2026-10-12 00:34:48 GRUS-1B
NORAD 47934
COSMOS 2581
NORAD 62902
4.154 14.67 1.0e-07
2026-10-12 03:49:38 GRUS-1B
NORAD 47934
DMSP 5D-3 F15 DEB
NORAD 26147
3.513 12.50 2.2e-07
2026-10-12 05:50:48 BISONSAT
NORAD 40974
GRUS-1B
NORAD 47934
3.941 4.44 2.7e-07
2026-10-12 07:56:09 GRUS-1B
NORAD 47934
OBJECT A
NORAD 69097
2.381 14.76 3.1e-07
2026-10-12 13:14:38 GRUS-1B
NORAD 47934
STARLINK-5897
NORAD 55931
4.243 6.87 6.7e-06
2026-10-12 17:02:02 GRUS-1B
NORAD 47934
STARLINK-36280
NORAD 67211
1.803 15.05 1.4e-05
2026-10-12 17:02:05 GRUS-1B
NORAD 47934
STARLINK-36270
NORAD 67200
2.503 15.05 7.4e-06
2026-10-13 06:46:28 GRUS-1B
NORAD 47934
STARLINK-5307
NORAD 55658
2.206 15.00 9.8e-06
2026-10-13 10:36:29 GRUS-1B
NORAD 47934
STARLINK-36185
NORAD 67204
3.439 15.06 3.9e-06
2026-10-13 21:18:40 GRUS-1B
NORAD 47934
SSB
NORAD 13845
3.705 13.00 1.9e-07
2026-10-14 04:10:59 GRUS-1B
NORAD 47934
STARLINK-36213
NORAD 67212
1.388 15.05 2.4e-05
2026-10-14 23:21:37 GRUS-1B
NORAD 47934
STARLINK-36283
NORAD 67197
3.521 15.04 3.8e-06
2026-10-15 02:26:43 GRUS-1B
NORAD 47934
STARLINK-5232
NORAD 55675
4.776 14.91 2.2e-06
2026-10-15 03:32:13 GRUS-1B
NORAD 47934
STARLINK-5067
NORAD 55653
2.837 15.05 5.8e-06
2026-10-15 08:24:40 GRUS-1B
NORAD 47934
STARLINK-6031
NORAD 56810
2.134 4.19 2.8e-05
2026-10-15 21:44:32 GRUS-1B
NORAD 47934
STARLINK-36197
NORAD 67205
2.840 15.01 5.9e-06
2026-10-16 16:17:34 GRUS-1B
NORAD 47934
STARLINK-5483
NORAD 55643
2.134 15.06 1.0e-05

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