SDGSAT 1
In orbit NORAD 49387 RGOT-7566-7340-2860-2308 China
2021
Launch
0
Observations all time
Gallery
1 49387U 21100A 26283.61647213 .00001607 00000-0 78578-4 0 9999
2 49387 97.2519 326.1067 0008011 219.3770 140.6884 15.19566931273447
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 |
|---|---|---|---|---|---|
| 2026-10-11 08:01:27 |
SDGSAT 1
NORAD 49387 |
STARLINK-4570
NORAD 53690 |
3.565 | 15.02 | 3.8e-06 |
| 2026-10-11 23:43:17 |
SBSS (USA 216)
NORAD 37168 |
SDGSAT 1
NORAD 49387 |
4.012 | 14.71 | 1.1e-07 |
| 2026-10-12 09:14:09 |
SDGSAT 1
NORAD 49387 |
STARLINK-3359
NORAD 51148 |
4.855 | 10.51 | 4.3e-06 |
| 2026-10-12 12:13:19 |
SDGSAT 1
NORAD 49387 |
BRO-20
NORAD 66674 |
3.785 | 3.69 | 3.0e-07 |
| 2026-10-12 13:02:12 |
SDGSAT 1
NORAD 49387 |
RASSVET-3 22
NORAD 100088 |
4.177 | 15.17 | 8.6e-08 |
| 2026-10-12 14:35:36 |
SDGSAT 1
NORAD 49387 |
BRO-20
NORAD 66674 |
3.800 | 3.70 | 3.0e-07 |
| 2026-10-12 14:37:04 |
SDGSAT 1
NORAD 49387 |
RASSVET-3 22
NORAD 100088 |
0.850 | 15.17 | 2.1e-06 |
| 2026-10-12 16:11:56 |
SDGSAT 1
NORAD 49387 |
RASSVET-3 22
NORAD 100088 |
2.691 | 15.17 | 2.1e-07 |
| 2026-10-12 17:30:43 |
SDGSAT 1
NORAD 49387 |
TIROS 8 DEB
NORAD 19396 |
3.353 | 14.71 | 1.6e-07 |
| 2026-10-12 23:05:22 |
SDGSAT 1
NORAD 49387 |
STARLINK-30145
NORAD 57496 |
3.902 | 11.78 | 6.0e-06 |
| 2026-10-13 00:57:27 |
STARLINK-3107
NORAD 49171 |
SDGSAT 1
NORAD 49387 |
3.164 | 13.03 | 7.9e-06 |
| 2026-10-13 02:52:31 |
SDGSAT 1
NORAD 49387 |
ROBUSTA-3A (MEDITERRANEE)
NORAD 60243 |
2.433 | 14.97 | 2.8e-07 |
| 2026-10-13 08:00:00 |
SDGSAT 1
NORAD 49387 |
RASSVET-3 30
NORAD 100096 |
4.896 | 15.15 | 6.3e-08 |
| 2026-10-13 09:34:52 |
SDGSAT 1
NORAD 49387 |
RASSVET-3 30
NORAD 100096 |
1.703 | 15.15 | 5.2e-07 |
| 2026-10-13 11:09:44 |
SDGSAT 1
NORAD 49387 |
RASSVET-3 30
NORAD 100096 |
2.817 | 15.15 | 1.9e-07 |
| 2026-10-13 15:55:10 |
SDGSAT 1
NORAD 49387 |
LUNA-2
NORAD 68470 |
3.101 | 10.28 | 3.5e-07 |
| 2026-10-14 13:54:33 |
SDGSAT 1
NORAD 49387 |
COSMOS 397 DEB
NORAD 5094 |
0.616 | 11.16 | 8.5e-06 |
| 2026-10-14 16:46:52 |
SDGSAT 1
NORAD 49387 |
STARLINK-3264
NORAD 50198 |
4.612 | 5.71 | 5.9e-06 |
| 2026-10-14 17:11:25 |
SDGSAT 1
NORAD 49387 |
CONNECTA IOT-15
NORAD 67402 |
4.330 | 5.79 | 2.2e-07 |
| 2026-10-14 23:29:15 |
SDGSAT 1
NORAD 49387 |
MICE-1
NORAD 66684 |
1.211 | 3.82 | 2.9e-06 |
| 2026-10-15 05:01:05 |
SDGSAT 1
NORAD 49387 |
MICE-1
NORAD 66684 |
1.498 | 3.81 | 1.9e-06 |
| 2026-10-15 09:07:34 |
SDGSAT 1
NORAD 49387 |
ATLAS 5 CENTAUR R/B
NORAD 40978 |
4.415 | 14.48 | 1.0e-07 |
| 2026-10-15 13:43:57 |
SDGSAT 1
NORAD 49387 |
RASSVET-3 32
NORAD 100098 |
1.499 | 15.09 | 7.0e-07 |
| 2026-10-15 15:18:49 |
SDGSAT 1
NORAD 49387 |
RASSVET-3 32
NORAD 100098 |
3.600 | 15.08 | 1.2e-07 |
| 2026-10-16 23:51:16 |
SDGSAT 1
NORAD 49387 |
UNKNOWN
NORAD 85237 |
3.731 | 14.78 | 1.3e-07 |
| 2026-10-17 00:51:54 |
SDGSAT 1
NORAD 49387 |
ELECTRON KICK STAGE R/B
NORAD 44636 |
3.193 | 15.36 | 1.5e-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.
