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GRUS-3A

In orbit NORAD 69885 LNTX-3600-1870-5043-8521

Observations 0
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Falcon 9 Block 5 | Transporter 17 (Dedicated SSO Rideshare)

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
GRUS-3A
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Launch
Falcon 9 Block 5 | Transporter 17 (Dedicated SSO Rideshare)
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
586.12 km
Apogee
594.04 km
Inclination
97.7°
Period
96.5 min
Semi-major axis
6968.2 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 69885U 26156S   26282.66795117  .00000923  00000-0  97628-4 0  9998
2 69885  97.7418 181.4665 0005683 173.7640 186.3651 14.91562656 14061
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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 21:28:52 GRUS-3A
NORAD 69885 		FENGYUN 1C DEB
NORAD 32432 		1.771 13.90 7.1e-07
2026-10-12 22:37:36 IRIDE-MS2-HEO-5
NORAD 64571 		GRUS-3A
NORAD 69885 		3.500 14.31 1.6e-07
2026-10-12 23:25:55 IRIDE-MS2-HEO-5
NORAD 64571 		GRUS-3A
NORAD 69885 		2.668 14.34 2.8e-07
2026-10-13 00:14:12 IRIDE-MS2-HEO-5
NORAD 64571 		GRUS-3A
NORAD 69885 		4.485 14.31 9.8e-08
2026-10-13 01:02:30 IRIDE-MS2-HEO-5
NORAD 64571 		GRUS-3A
NORAD 69885 		1.681 14.34 7.0e-07
2026-10-13 22:15:15 GRUS-3A
NORAD 69885 		FENGYUN 1C DEB
NORAD 30546 		2.579 0.16 6.6e-07
2026-10-13 23:51:57 GRUS-3A
NORAD 69885 		FENGYUN 1C DEB
NORAD 30546 		4.714 0.16 2.0e-07
2026-10-14 10:48:00 GRUS-3A
NORAD 69885 		COROT
NORAD 29678 		1.883 14.56 5.3e-07
2026-10-16 06:17:37 GRUS-3A
NORAD 69885 		COSMOS 2251 DEB
NORAD 33999 		4.277 14.46 1.0e-07
2026-10-16 19:24:35 GRUS-3A
NORAD 69885 		CZ-6A DEB
NORAD 54576 		4.970 14.95 6.5e-08
2026-10-16 23:57:05 GRUS-3A
NORAD 69885 		FENGYUN 1C DEB
NORAD 29982 		4.834 3.52 1.8e-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