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OBJECT G

In orbit NORAD 100471 ALXQ-7468-7756-2633-1586

Observations 0
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Long March 6C | 7 satellites

Long March 6C

Carrier rocket

Launch Complex 9A

Spaceport

0

Observations all time

Mission information
Spacecraft name
OBJECT G
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Launch
Long March 6C | 7 satellites
Carrier rocket
Long March 6C
Spaceport
Launch Complex 9A
Launch time
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
526.41 km
Apogee
543.64 km
Inclination
97.5°
Period
95.4 min
Semi-major axis
6913.2 km
Velocity
7.6 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-15 10:09:06 UTC
Two-line elements (TLE)
1 A0471U 26195G   26287.49854541  .00004307  00000-0  27299-3 0  9996
2 A0471  97.5270   0.4117 0012488 106.0499 254.2106 15.09400020  7603
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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
2026-10-15 17:52:55 OBJECT G
NORAD 100471 		COSMOS 2251 DEB
NORAD 35043 		0.810 14.66 2.8e-06
2026-10-17 00:40:40 STARLINK-5317
NORAD 55283 		OBJECT G
NORAD 100471 		2.754 14.85 6.9e-06
2026-10-17 02:16:02 STARLINK-5317
NORAD 55283 		OBJECT G
NORAD 100471 		1.659 14.85 1.9e-05
2026-10-17 05:49:28 STARLINK-30845
NORAD 58207 		OBJECT G
NORAD 100471 		4.364 9.38 5.7e-06
2026-10-17 22:13:36 OBJECT G
NORAD 100471 		PEGASUS DEB
NORAD 24236 		4.696 15.21 6.7e-08
2026-10-18 17:26:42 OBJECT G
NORAD 100471 		FENGYUN 1C DEB
NORAD 30017 		4.073 0.79 2.6e-07
2026-10-19 04:06:14 STARLINK-4769
NORAD 53843 		OBJECT G
NORAD 100471 		2.879 5.76 1.5e-05
2026-10-19 04:33:56 OBJECT G
NORAD 100471 		PEGASUS DEB
NORAD 24197 		3.774 15.16 1.0e-07
2026-10-19 09:53:58 STARLINK-5317
NORAD 55283 		OBJECT G
NORAD 100471 		1.723 15.01 1.6e-05
2026-10-19 11:29:20 STARLINK-5317
NORAD 55283 		OBJECT G
NORAD 100471 		3.334 15.01 4.4e-06
2026-10-20 05:03:26 OBJECT G
NORAD 100471 		COSMOS 2058
NORAD 20465 		3.814 15.20 1.0e-07
2026-10-20 17:26:31 STARLINK-5059
NORAD 53912 		OBJECT G
NORAD 100471 		2.832 6.03 1.5e-05
2026-10-20 19:49:43 STARLINK-5059
NORAD 53912 		OBJECT G
NORAD 100471 		3.520 6.02 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