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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

Mission information
Spacecraft name
LEMUR-2-FINNIAN
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
554.19 km
Apogee
566.00 km
Inclination
97.5°
Period
95.9 min
Semi-major axis
6938.2 km
Velocity
7.56 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 14:09:05 UTC
Two-line elements (TLE)
1 66782U 25276DW  26287.15737644  .00004992  00000-0  39286-3 0  9998
2 66782 97.5137 354.4314 0008509 63.2219 296.9876 15.01230136 37843
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Orbit history, past year

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.

Prediction divergence

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
2026-10-15 15:58:14 STARLINK-5285
NORAD 55296
LEMUR-2-FINNIAN
NORAD 66782
3.484 14.94 4.0e-06
2026-10-15 21:33:11 QPS-SAR-11 (YAMATSUMI-I)
NORAD 64340
LEMUR-2-FINNIAN
NORAD 66782
2.503 12.36 4.5e-07
2026-10-16 00:17:35 STARLINK-5989
NORAD 56781
LEMUR-2-FINNIAN
NORAD 66782
3.831 14.64 3.7e-06
2026-10-16 04:36:28 LEMUR-2-FINNIAN
NORAD 66782
STARLINK-36222
NORAD 67097
4.139 15.05 2.7e-06
2026-10-16 17:40:44 LEMUR-2-FINNIAN
NORAD 66782
STARLINK-36209
NORAD 67022
4.757 11.74 4.0e-06
2026-10-16 22:28:25 STARLINK-5605
NORAD 55411
LEMUR-2-FINNIAN
NORAD 66782
3.187 13.72 6.8e-06
2026-10-17 01:34:06 LEMUR-2-FINNIAN
NORAD 66782
NOAA 16 DEB
NORAD 41363
2.965 14.81 1.9e-07
2026-10-17 07:53:51 STARLINK-5308
NORAD 55300
LEMUR-2-FINNIAN
NORAD 66782
3.215 15.01 4.6e-06
2026-10-17 18:53:34 LEMUR-2-FINNIAN
NORAD 66782
STARLINK-36170
NORAD 67083
4.895 15.06 1.9e-06
2026-10-17 22:35:39 LEMUR-2-FINNIAN
NORAD 66782
FENGYUN 1C DEB
NORAD 36695
2.256 10.67 6.5e-07
2026-10-17 23:51:30 STARLINK-5318
NORAD 55304
LEMUR-2-FINNIAN
NORAD 66782
2.975 15.03 5.3e-06
2026-10-18 05:54:30 LEMUR-2-FINNIAN
NORAD 66782
COSMOS 397 DEB
NORAD 5017
2.204 14.81 3.9e-07
2026-10-18 08:42:05 YAOGAN-30 03C
NORAD 43030
LEMUR-2-FINNIAN
NORAD 66782
4.820 12.63 1.2e-07
2026-10-18 09:43:15 LEMUR-2-FINNIAN
NORAD 66782
PEGASUS DEB
NORAD 24236
4.480 15.14 7.5e-08
2026-10-19 04:52:05 LEMUR-2-FINNIAN
NORAD 66782
STARLINK-36106
NORAD 67018
3.527 12.38 6.8e-06
2026-10-19 21:18:55 YAOGAN-30 07A
NORAD 45460
LEMUR-2-FINNIAN
NORAD 66782
4.692 13.85 1.0e-07
2026-10-20 03:19:52 LEMUR-2-FINNIAN
NORAD 66782
COSMOS 2151
NORAD 21422
4.152 13.89 1.3e-07
2026-10-20 04:55:52 LEMUR-2-FINNIAN
NORAD 66782
COSMOS 2151
NORAD 21422
3.316 13.90 2.0e-07
2026-10-20 05:43:49 LEMUR-2-FINNIAN
NORAD 66782
COSMOS 2151
NORAD 21422
1.640 13.95 8.2e-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.

All conjunctions of this satellite