GAOFEN 8
In orbit NORAD 40701 EBQW-3809-5107-3366-2488 China
2015
Launch
0
Observations all time
Gallery
1 40701U 15030A 26285.99746455 .00025869 00000-0 46213-3 0 9992
2 40701 97.6800 126.7753 0009035 120.4824 239.7320 15.49980810629674
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.
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 |
|---|---|---|---|---|---|
| 2026-10-16 05:03:47 |
GAOFEN-8
NORAD 40701 |
DEIMOS
NORAD 60526 |
2.361 | 12.61 | 5.0e-07 |
| 2026-10-16 06:26:36 |
GAOFEN-8
NORAD 40701 |
COSMOS 1408 DEB
NORAD 50032 |
3.370 | 4.15 | 3.8e-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.
