Conjunctions
Close approaches within 5 km between satellites in the portal catalog and other objects in orbit over the next seven days. The table is updated three times a day.
Last updated, UTC: 2026-10-10 16:30
Last updated, UTC: 2026-10-10 16:30
| Time of closest approach, UTC | Object 1 | Object 2 | Distance, km | Speed, km/s | Max. probability |
|---|---|---|---|---|---|
| 2026-10-15 13:50:44 |
STARLINK-6085
NORAD 57115 |
IRIDE-MS1-EAGLET 2-2
NORAD 66696 |
4.279 | 12.88 | 4.4e-06 |
| 2026-10-16 00:39:38 |
IRIDE-MS1-EAGLET 2-2
NORAD 66696 |
OBJECT B
NORAD 67747 |
1.446 | 7.08 | 1.9e-06 |
| 2026-10-13 10:51:41 |
TOMORROW-S9
NORAD 66309 |
IRIDE-MS1-EAGLET 2-2
NORAD 66696 |
1.434 | 14.08 | 1.1e-06 |
| 2026-10-15 20:47:48 |
HORUS 1
NORAD 55690 |
IRIDE-MS1-EAGLET 2-2
NORAD 66696 |
3.294 | 0.04 | 4.1e-07 |
| 2026-10-12 19:08:15 |
HXMT (HUIYAN)
NORAD 42758 |
IRIDE-MS1-EAGLET 2-2
NORAD 66696 |
3.601 | 12.40 | 2.2e-07 |
| 2026-10-13 23:23:37 |
LIZZIESAT-3 (LS-3)
NORAD 63233 |
IRIDE-MS1-EAGLET 2-2
NORAD 66696 |
2.722 | 15.10 | 2.1e-07 |
| 2026-10-16 12:17:58 |
IRIDE-MS1-EAGLET 2-2
NORAD 66696 |
HULIANWANG JISHU SHIYAN 9C
NORAD 68833 |
3.318 | 14.33 | 1.8e-07 |
| 2026-10-11 13:41:16 |
IRIDE-MS1-EAGLET 2-2
NORAD 66696 |
GEN1A-2
NORAD 69005 |
3.177 | 15.09 | 1.6e-07 |
| 2026-10-16 20:12:15 |
HULIANWANG JISHU SHIYAN 6D
NORAD 63431 |
IRIDE-MS1-EAGLET 2-2
NORAD 66696 |
4.162 | 14.20 | 1.2e-07 |
| 2026-10-14 00:58:17 |
LIZZIESAT-3 (LS-3)
NORAD 63233 |
IRIDE-MS1-EAGLET 2-2
NORAD 66696 |
3.693 | 15.10 | 1.1e-07 |
| 2026-10-14 03:20:18 |
LIZZIESAT-3 (LS-3)
NORAD 63233 |
IRIDE-MS1-EAGLET 2-2
NORAD 66696 |
3.881 | 15.09 | 1.0e-07 |
| 2026-10-11 12:06:33 |
IRIDE-MS1-EAGLET 2-2
NORAD 66696 |
GEN1A-2
NORAD 69005 |
3.899 | 15.09 | 1.0e-07 |
| 2026-10-11 15:15:59 |
IRIDE-MS1-EAGLET 2-2
NORAD 66696 |
GEN1A-2
NORAD 69005 |
4.367 | 15.09 | 8.2e-08 |
| 2026-10-14 04:54:58 |
LIZZIESAT-3 (LS-3)
NORAD 63233 |
IRIDE-MS1-EAGLET 2-2
NORAD 66696 |
4.488 | 15.09 | 7.8e-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.