LEMUR-2-FINNIAN
In orbit NORAD 66782 VXCD-3740-2953-4946-8253
Falcon 9 Block 5
Carrier rocket
Space Launch Complex 4E
Spaceport
0
Observations all time
The satellite is in orbit
The network has not received data from this satellite for a long time
Gallery
1 66782U 25276DW 26282.95812256 .00004963 00000-0 39112-3 0 9990
2 66782 97.5162 350.3688 0008996 76.4299 283.7927 15.01177885 37217
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 06:25:45 |
LEMUR-2-FINNIAN
NORAD 66782 |
STARLINK-36193
NORAD 67099 |
3.405 | 14.84 | 4.4e-06 |
| 2026-10-12 08:57:13 |
OBJECT L
NORAD 61904 |
LEMUR-2-FINNIAN
NORAD 66782 |
3.998 | 0.13 | 2.7e-07 |
| 2026-10-12 09:35:52 |
LEMUR-2-FINNIAN
NORAD 66782 |
STARLINK-36159
NORAD 67079 |
0.879 | 14.91 | 6.4e-05 |
| 2026-10-12 13:43:28 |
KHALIFASAT
NORAD 43676 |
LEMUR-2-FINNIAN
NORAD 66782 |
1.797 | 13.01 | 8.0e-07 |
| 2026-10-12 14:31:27 |
KHALIFASAT
NORAD 43676 |
LEMUR-2-FINNIAN
NORAD 66782 |
4.405 | 12.96 | 1.3e-07 |
| 2026-10-12 14:42:53 |
LEMUR-2-FINNIAN
NORAD 66782 |
STARLINK-36084
NORAD 66829 |
3.200 | 14.69 | 5.2e-06 |
| 2026-10-12 15:19:26 |
KHALIFASAT
NORAD 43676 |
LEMUR-2-FINNIAN
NORAD 66782 |
4.464 | 13.01 | 1.3e-07 |
| 2026-10-12 16:07:25 |
KHALIFASAT
NORAD 43676 |
LEMUR-2-FINNIAN
NORAD 66782 |
4.520 | 12.96 | 1.3e-07 |
| 2026-10-13 09:33:44 |
LEMUR-2-FINNIAN
NORAD 66782 |
STARLINK-36158
NORAD 67080 |
3.774 | 14.97 | 3.4e-06 |
| 2026-10-13 09:38:01 |
STARLINK-5284
NORAD 55297 |
LEMUR-2-FINNIAN
NORAD 66782 |
1.060 | 14.78 | 4.6e-05 |
| 2026-10-13 13:46:42 |
LEMUR-2-FINNIAN
NORAD 66782 |
UNKNOWN
NORAD 270443 |
3.787 | 11.26 | 2.2e-07 |
| 2026-10-13 22:20:06 |
STARLINK-5232
NORAD 55675 |
LEMUR-2-FINNIAN
NORAD 66782 |
1.082 | 4.42 | 1.1e-04 |
| 2026-10-14 05:05:31 |
LEMUR-2-FINNIAN
NORAD 66782 |
STARLINK-35838
NORAD 66836 |
2.720 | 14.52 | 7.7e-06 |
| 2026-10-14 12:53:17 |
LEMUR-2-FINNIAN
NORAD 66782 |
STARLINK-35498
NORAD 67017 |
1.672 | 11.12 | 3.4e-05 |
| 2026-10-14 14:37:03 |
SHIJIAN-6 05A (SJ-6 05A)
NORAD 49961 |
LEMUR-2-FINNIAN
NORAD 66782 |
1.216 | 11.84 | 2.0e-06 |
| 2026-10-14 16:16:19 |
STARLINK-5899
NORAD 55949 |
LEMUR-2-FINNIAN
NORAD 66782 |
4.386 | 9.82 | 5.5e-06 |
| 2026-10-14 19:17:22 |
STARLINK-5074
NORAD 55438 |
LEMUR-2-FINNIAN
NORAD 66782 |
2.007 | 13.33 | 1.8e-05 |
| 2026-10-14 23:53:16 |
LEMUR-2-FINNIAN
NORAD 66782 |
STARLINK-35882
NORAD 67088 |
2.327 | 15.03 | 8.7e-06 |
| 2026-10-15 21:33:17 |
QPS-SAR-11 (YAMATSUMI-I)
NORAD 64340 |
LEMUR-2-FINNIAN
NORAD 66782 |
3.889 | 12.37 | 1.9e-07 |
| 2026-10-16 09:36:29 |
SSTL S1-4
NORAD 43618 |
LEMUR-2-FINNIAN
NORAD 66782 |
4.604 | 14.75 | 8.2e-08 |
| 2026-10-16 09:51:06 |
STARLINK-3078
NORAD 49134 |
LEMUR-2-FINNIAN
NORAD 66782 |
4.159 | 11.85 | 5.2e-06 |
| 2026-10-16 18:57:59 |
LEMUR-2-FINNIAN
NORAD 66782 |
STARLINK-35841
NORAD 67086 |
4.658 | 15.06 | 2.1e-06 |
| 2026-10-16 20:46:18 |
LEMUR-2-FINNIAN
NORAD 66782 |
NOAA 16 DEB
NORAD 41363 |
4.900 | 14.81 | 7.1e-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.
