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: 2026-10-12 16:30
Last updated, UTC: 2026-10-12 16:30
| Time of closest approach, UTC | Object 1 | Object 2 | Distance, km | Speed, km/s | Max. probability |
|---|---|---|---|---|---|
| 2026-10-14 06:03:59 |
HERMES-5
NORAD 63834 |
STARLINK-38248
NORAD 100435 |
4.334 | 15.11 | 2.6e-06 |
| 2026-10-15 20:12:26 |
STARLINK-30435
NORAD 57842 |
HERMES-5
NORAD 63834 |
4.933 | 14.52 | 2.4e-06 |
| 2026-10-17 03:36:47 |
FLOCK 4G-34
NORAD 62650 |
HERMES-5
NORAD 63834 |
1.077 | 15.10 | 1.4e-06 |
| 2026-10-17 22:41:47 |
SVYATOBOR 1 (RS60S)
NORAD 57187 |
HERMES-5
NORAD 63834 |
1.169 | 15.06 | 1.2e-06 |
| 2026-10-14 23:08:23 |
TOMORROW-S3
NORAD 62392 |
HERMES-5
NORAD 63834 |
1.603 | 14.43 | 7.8e-07 |
| 2026-10-18 04:43:16 |
FLOCK 4G-6
NORAD 62660 |
HERMES-5
NORAD 63834 |
2.743 | 15.10 | 2.1e-07 |
| 2026-10-14 12:05:01 |
STARLINK-33705
NORAD 63651 |
HERMES-5
NORAD 63834 |
4.439 | 7.60 | 2.0e-07 |
| 2026-10-17 20:11:04 |
STARLINK-33661
NORAD 63646 |
HERMES-5
NORAD 63834 |
4.639 | 7.00 | 1.9e-07 |
| 2026-10-17 05:10:54 |
FLOCK 4G-34
NORAD 62650 |
HERMES-5
NORAD 63834 |
3.063 | 15.10 | 1.7e-07 |
| 2026-10-17 02:02:39 |
FLOCK 4G-34
NORAD 62650 |
HERMES-5
NORAD 63834 |
3.545 | 15.10 | 1.3e-07 |
| 2026-10-16 08:05:35 |
OBJECT C
NORAD 59679 |
HERMES-5
NORAD 63834 |
3.748 | 15.12 | 1.1e-07 |
| 2026-10-16 22:07:22 |
FLOCK 4G-34
NORAD 62650 |
HERMES-5
NORAD 63834 |
3.838 | 15.09 | 1.1e-07 |
| 2026-10-14 23:08:25 |
HERMES-5
NORAD 63834 |
SHIYAN-33
NORAD 68405 |
3.953 | 15.13 | 1.0e-07 |
| 2026-10-16 23:41:29 |
FLOCK 4G-34
NORAD 62650 |
HERMES-5
NORAD 63834 |
4.106 | 15.09 | 9.4e-08 |
| 2026-10-18 03:09:09 |
FLOCK 4G-6
NORAD 62660 |
HERMES-5
NORAD 63834 |
4.138 | 15.10 | 9.3e-08 |
| 2026-10-18 00:48:01 |
FLOCK 4G-6
NORAD 62660 |
HERMES-5
NORAD 63834 |
4.851 | 15.09 | 6.7e-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.