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

LEMUR-2-VUKASIN

In orbit NORAD 66785 KRUW-8555-8781-8249-7141

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
LEMUR-2-VUKASIN
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
556.44 km
Apogee
564.03 km
Inclination
97.5°
Period
95.9 min
Semi-major axis
6938.4 km
Velocity
7.58 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 12:56:45 UTC
Two-line elements (TLE)
1 66785U 25276DZ  26284.17547007  .00006458  00000-0  50766-3 0  9997
2 66785 97.4979 351.2594 0005446 75.9717 284.2113 15.01185952 47541
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
2026-10-12 05:16:12 SMDC ONE 2.4
NORAD 39469
LEMUR-2-VUKASIN
NORAD 66785
2.550 10.53 5.1e-07
2026-10-12 16:24:47 LEMUR-2-VUKASIN
NORAD 66785
STARLINK-35842
NORAD 67087
4.071 14.93 3.0e-06
2026-10-12 21:31:58 LEMUR-2-VUKASIN
NORAD 66785
STARLINK-36073
NORAD 66844
4.565 14.67 2.6e-06
2026-10-12 21:54:57 LEMUR-2-VUKASIN
NORAD 66785
KUIPER-00555
NORAD 69620
2.243 14.48 3.8e-07
2026-10-12 23:07:55 LEMUR-2-VUKASIN
NORAD 66785
STARLINK-35959
NORAD 66827
4.248 14.66 3.0e-06
2026-10-13 00:27:40 STARLINK-34604
NORAD 64801
LEMUR-2-VUKASIN
NORAD 66785
4.127 6.80 7.1e-06
2026-10-14 08:26:32 STARLINK-5987
NORAD 56455
LEMUR-2-VUKASIN
NORAD 66785
2.323 6.27 2.3e-05
2026-10-14 14:24:43 LEMUR-2-VUKASIN
NORAD 66785
ELECTRON KICK STAGE R/B
NORAD 65117
3.307 10.71 3.0e-07
2026-10-15 06:59:40 LEMUR-2-VUKASIN
NORAD 66785
OBJECT F
NORAD 100614
1.534 0.90 1.9e-06
2026-10-16 01:07:04 GEESAT-1 05
NORAD 52789
LEMUR-2-VUKASIN
NORAD 66785
3.640 7.05 3.0e-07
2026-10-16 22:07:07 LEMUR-2-VUKASIN
NORAD 66785
SL-8 R/B
NORAD 3230
3.538 14.05 8.5e-07
2026-10-17 01:59:42 STARLINK-5456
NORAD 55667
LEMUR-2-VUKASIN
NORAD 66785
2.326 5.29 2.3e-05
2026-10-17 06:10:41 UM5-RIBAT
NORAD 60554
LEMUR-2-VUKASIN
NORAD 66785
4.962 1.19 1.8e-07
2026-10-17 06:58:41 UM5-RIBAT
NORAD 60554
LEMUR-2-VUKASIN
NORAD 66785
4.342 1.19 2.3e-07
2026-10-17 07:46:39 UM5-RIBAT
NORAD 60554
LEMUR-2-VUKASIN
NORAD 66785
3.984 1.19 2.8e-07
2026-10-17 08:30:01 LEMUR-2-VUKASIN
NORAD 66785
STARLINK-36172
NORAD 67020
4.680 11.87 4.1e-06

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