RU | EN | ZH --:-- UTC Sign in

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
494.80 km
Apogee
497.95 km
Inclination
97.4°
Period
94.6 min
Semi-major axis
6874.5 km
Velocity
7.62 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 14:09:05 UTC
Two-line elements (TLE)
1 66768U 25276DG  26287.27615581  .00005579  00000-0  24641-3 0  9991
2 66768 97.4042 359.2238 0002292 96.7673 263.3825 15.22130467 48558
Copy content
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 20:08:54 LEMUR-2-TEODOR
NORAD 66768
SARAMAGO
NORAD 100000
3.961 12.68 1.7e-07
2026-10-15 20:56:13 LEMUR-2-TEODOR
NORAD 66768
SARAMAGO
NORAD 100000
4.921 12.70 1.1e-07
2026-10-15 21:43:34 LEMUR-2-TEODOR
NORAD 66768
SARAMAGO
NORAD 100000
3.447 12.68 2.3e-07
2026-10-16 19:40:54 STARLINK-5598
NORAD 55421
LEMUR-2-TEODOR
NORAD 66768
2.074 12.97 1.8e-05
2026-10-16 21:23:29 LEMUR-2-TEODOR
NORAD 66768
R5-S10
NORAD 100801
0.695 12.63 5.7e-06
2026-10-17 19:51:32 TRANSPORTER-13 OBJECT M
NORAD 63221
LEMUR-2-TEODOR
NORAD 66768
3.689 15.10 1.2e-07
2026-10-17 21:26:11 TRANSPORTER-13 OBJECT M
NORAD 63221
LEMUR-2-TEODOR
NORAD 66768
1.900 15.10 4.3e-07
2026-10-17 23:00:49 TRANSPORTER-13 OBJECT M
NORAD 63221
LEMUR-2-TEODOR
NORAD 66768
0.387 15.10 1.0e-05
2026-10-18 00:35:28 TRANSPORTER-13 OBJECT M
NORAD 63221
LEMUR-2-TEODOR
NORAD 66768
1.794 15.10 4.9e-07
2026-10-18 02:10:07 TRANSPORTER-13 OBJECT M
NORAD 63221
LEMUR-2-TEODOR
NORAD 66768
3.579 15.10 1.2e-07
2026-10-18 03:29:10 LEMUR-2-TEODOR
NORAD 66768
SL-24 R/B
NORAD 36606
3.017 15.03 1.9e-07
2026-10-18 04:32:06 TRANSPORTER-13 OBJECT M
NORAD 63221
LEMUR-2-TEODOR
NORAD 66768
4.774 15.10 6.9e-08
2026-10-18 06:06:45 TRANSPORTER-13 OBJECT M
NORAD 63221
LEMUR-2-TEODOR
NORAD 66768
3.423 15.10 1.3e-07
2026-10-18 07:41:23 TRANSPORTER-13 OBJECT M
NORAD 63221
LEMUR-2-TEODOR
NORAD 66768
2.673 15.10 2.2e-07
2026-10-18 09:16:02 TRANSPORTER-13 OBJECT M
NORAD 63221
LEMUR-2-TEODOR
NORAD 66768
3.012 15.10 1.7e-07
2026-10-18 10:50:41 TRANSPORTER-13 OBJECT M
NORAD 63221
LEMUR-2-TEODOR
NORAD 66768
4.182 15.10 9.0e-08
2026-10-19 02:12:21 FLOCK 4H-8
NORAD 66711
LEMUR-2-TEODOR
NORAD 66768
4.444 0.02 2.2e-07
2026-10-19 12:26:56 SKYBEE-A01
NORAD 62671
LEMUR-2-TEODOR
NORAD 66768
2.896 0.59 5.3e-07
2026-10-20 09:45:13 SNUSAT-2
NORAD 43782
LEMUR-2-TEODOR
NORAD 66768
1.606 2.67 1.7e-06
2026-10-20 23:08:55 LEMUR-2-TEODOR
NORAD 66768
ALSAT-3A
NORAD 67474
3.365 0.14 3.9e-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