SAUDISAT 1C
In orbit NORAD 27607 IRES-5964-9687-1982-0089 Saudi Arabia
Time in UTC
20:54
Next pass · Чукотка · 22°
11.10 11:39
Scheduled · Обозерский
14
Observations over 30 days
28%
Successful observations
1
Frames, latest 2025-04-19 19:31 UTC
Saudi Arabian amateur radio satellite
The satellite is in orbit
Gallery
1 27607U 02058C 26282.91694023 .00000669 00000-0 96602-4 0 9999
2 27607 64.5510 133.9581 0070456 241.2598 118.1417 14.83247631281472
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 |
|---|---|---|---|---|---|
| 2026-10-10 23:42:49 |
SAUDISAT 1C (SO-50)
NORAD 27607 |
FENGYUN 1C DEB
NORAD 38169 |
4.109 | 14.85 | 9.8e-08 |
| 2026-10-11 06:46:59 |
SAUDISAT 1C (SO-50)
NORAD 27607 |
ALOS (DAICHI)
NORAD 28931 |
1.962 | 12.42 | 7.2e-07 |
| 2026-10-11 11:59:36 |
SAUDISAT 1C (SO-50)
NORAD 27607 |
SL-24 DEB
NORAD 33398 |
3.369 | 14.95 | 1.4e-07 |
| 2026-10-11 14:22:02 |
SAUDISAT 1C (SO-50)
NORAD 27607 |
COSMOS 2251 DEB
NORAD 47119 |
4.278 | 14.02 | 1.2e-07 |
| 2026-10-11 21:17:53 |
SAUDISAT 1C (SO-50)
NORAD 27607 |
MICROCARB
NORAD 64899 |
4.634 | 13.46 | 1.1e-07 |
| 2026-10-12 01:08:54 |
SAUDISAT 1C (SO-50)
NORAD 27607 |
STARLINK-5459
NORAD 55669 |
3.423 | 13.46 | 6.2e-06 |
| 2026-10-12 09:25:33 |
SAUDISAT 1C (SO-50)
NORAD 27607 |
STARLINK-35840
NORAD 66834 |
3.377 | 2.71 | 1.2e-05 |
| 2026-10-12 14:21:59 |
SAUDISAT 1C (SO-50)
NORAD 27607 |
LEMUR-2-HUBBLE-5
NORAD 64840 |
4.854 | 10.74 | 1.4e-07 |
| 2026-10-12 18:59:16 |
SAUDISAT 1C (SO-50)
NORAD 27607 |
STARLINK-36263
NORAD 67202 |
2.645 | 13.05 | 1.1e-05 |
| 2026-10-12 19:23:24 |
SAUDISAT 1C (SO-50)
NORAD 27607 |
UNKNOWN
NORAD 270309 |
2.819 | 14.80 | 2.1e-07 |
| 2026-10-13 09:20:51 |
SAUDISAT 1C (SO-50)
NORAD 27607 |
CZ-4C DEB
NORAD 39212 |
4.759 | 14.96 | 7.1e-08 |
| 2026-10-13 14:26:18 |
SAUDISAT 1C (SO-50)
NORAD 27607 |
STARLINK-5495
NORAD 55635 |
2.738 | 12.55 | 1.1e-05 |
| 2026-10-14 13:01:35 |
SAUDISAT 1C (SO-50)
NORAD 27607 |
STARLINK-5328
NORAD 55657 |
2.625 | 13.41 | 1.1e-05 |
| 2026-10-14 13:44:35 |
SAUDISAT 1C (SO-50)
NORAD 27607 |
NOAA 17 DEB
NORAD 48734 |
2.414 | 14.86 | 2.7e-07 |
| 2026-10-15 04:51:15 |
SAUDISAT 1C (SO-50)
NORAD 27607 |
KUIPER-00386
NORAD 68921 |
4.983 | 11.40 | 1.2e-07 |
| 2026-10-15 08:13:25 |
SAUDISAT 1C (SO-50)
NORAD 27607 |
FREGAT DEB
NORAD 46411 |
1.872 | 13.17 | 7.7e-07 |
| 2026-10-15 11:53:38 |
SAUDISAT 1C (SO-50)
NORAD 27607 |
SATELIOT_1
NORAD 60550 |
4.868 | 12.79 | 1.1e-07 |
| 2026-10-15 13:46:43 |
SAUDISAT 1C (SO-50)
NORAD 27607 |
AETHER-5
NORAD 67376 |
4.338 | 14.85 | 8.8e-08 |
| 2026-10-15 16:36:17 |
SAUDISAT 1C (SO-50)
NORAD 27607 |
STARLINK-5065
NORAD 55641 |
2.963 | 12.47 | 9.6e-06 |
| 2026-10-15 17:48:09 |
SAUDISAT 1C (SO-50)
NORAD 27607 |
KUIPER-00166
NORAD 65779 |
2.592 | 2.29 | 6.5e-07 |
| 2026-10-16 15:11:33 |
SAUDISAT 1C (SO-50)
NORAD 27607 |
STARLINK-5456
NORAD 55667 |
1.544 | 13.37 | 3.1e-05 |
| 2026-10-17 00:38:43 |
SAUDISAT 1C (SO-50)
NORAD 27607 |
AETHER-12
NORAD 67383 |
4.660 | 14.92 | 7.4e-08 |
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.
