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LEMUR-2-TEODOR

In orbit NORAD 66768 KWYJ-3242-8750-7758-3479

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
LEMUR-2-TEODOR
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
494.92 km
Apogee
498.07 km
Inclination
97.4°
Period
94.6 min
Semi-major axis
6874.6 km
Velocity
7.6 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 04:56:40 UTC
Two-line elements (TLE)
1 66768U 25276DG  26283.92340096  .00007057  00000-0  31118-3 0  9995
2 66768 97.4054 355.9225 0002293 100.5519 259.5976 15.22091255 48043
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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
2026-10-11 12:46:14 HORUS 2
NORAD 55844
LEMUR-2-TEODOR
NORAD 66768
3.761 0.13 3.1e-07
2026-10-11 14:20:24 SPAWAR-CAL-OR
NORAD 43778
LEMUR-2-TEODOR
NORAD 66768
2.259 3.35 8.5e-07
2026-10-12 10:50:16 IRIDE-MS1-EAGLET 2-6
NORAD 66700
LEMUR-2-TEODOR
NORAD 66768
1.145 0.04 3.4e-06
2026-10-12 11:37:33 IRIDE-MS1-EAGLET 2-6
NORAD 66700
LEMUR-2-TEODOR
NORAD 66768
2.543 0.04 6.8e-07
2026-10-13 12:40:29 LEMUR-2-TEODOR
NORAD 66768
LPNTSAT-001 (IOD-1)
NORAD 68408
4.111 14.97 9.7e-08
2026-10-13 19:57:52 GHGSAT-C13
NORAD 64548
LEMUR-2-TEODOR
NORAD 66768
1.889 5.50 1.2e-06
2026-10-13 20:06:55 LEMUR-2-TEODOR
NORAD 66768
FENGYUN 1C DEB
NORAD 29771
2.266 14.64 3.6e-07
2026-10-13 21:32:32 GHGSAT-C13
NORAD 64548
LEMUR-2-TEODOR
NORAD 66768
1.390 5.50 2.1e-06
2026-10-13 22:19:52 GHGSAT-C13
NORAD 64548
LEMUR-2-TEODOR
NORAD 66768
2.315 5.49 7.7e-07
2026-10-13 23:07:11 GHGSAT-C13
NORAD 64548
LEMUR-2-TEODOR
NORAD 66768
4.565 5.50 2.0e-07
2026-10-13 23:54:31 GHGSAT-C13
NORAD 64548
LEMUR-2-TEODOR
NORAD 66768
0.992 5.49 4.2e-06
2026-10-14 01:29:11 GHGSAT-C13
NORAD 64548
LEMUR-2-TEODOR
NORAD 66768
4.134 5.49 2.4e-07
2026-10-14 03:04:43 TRANSPORTER-15 OBJECT AA
NORAD 66690
LEMUR-2-TEODOR
NORAD 66768
3.916 0.10 2.9e-07
2026-10-14 03:56:20 LEMUR-2-TEODOR
NORAD 66768
CZ-2C DEB
NORAD 37770
4.516 13.76 1.1e-07
2026-10-14 23:35:51 LEMUR-2-TEODOR
NORAD 66768
OBJECT K
NORAD 49404
1.520 4.38 1.8e-06
2026-10-15 20:08:57 LEMUR-2-TEODOR
NORAD 66768
SARAMAGO
NORAD 100000
2.979 12.68 3.1e-07
2026-10-15 20:56:16 LEMUR-2-TEODOR
NORAD 66768
SARAMAGO
NORAD 100000
4.599 12.70 1.3e-07
2026-10-15 21:43:38 LEMUR-2-TEODOR
NORAD 66768
SARAMAGO
NORAD 100000
4.481 12.68 1.4e-07
2026-10-16 15:01:46 TIANHUI 1-04
NORAD 49049
LEMUR-2-TEODOR
NORAD 66768
4.525 0.99 2.2e-07
2026-10-16 15:02:21 FLOCK 4H-16
NORAD 66719
LEMUR-2-TEODOR
NORAD 66768
3.846 0.03 3.0e-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