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LASARsat

In orbit NORAD 62391 LLUY-1732-6975-8970-4189

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

341

Observations all time

Mission information
Spacecraft name
LASARsat
Other names
OK0LSR
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
2024-12-21 11:34:00
Separation time
Last observers
Observer
Time of receipt
2025-12-04 17:58:10 UTC
2025-12-04 16:17:57 UTC
2025-12-03 16:53:20 UTC
2025-12-02 15:48:51 UTC
2025-11-30 20:09:40 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
400.56 km
Apogee
412.91 km
Inclination
45.0°
Period
92.7 min
Semi-major axis
6784.9 km
Velocity
7.66 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 04:56:39 UTC
Two-line elements (TLE)
1 62391U 24247Q   26283.85316482  .00064451  00000-0  96985-3 0  9998
2 62391 44.9724 328.6653 0009101 355.8229 4.2587 15.53984660101264
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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
2026-10-12 02:51:15 NUSAT-39 (TIKVAH ALPER)
NORAD 56201
LASARSAT
NORAD 62391
4.002 13.23 1.6e-07
2026-10-12 23:11:34 LASARSAT
NORAD 62391
HOKUSHIN-1
NORAD 69648
3.043 9.81 3.8e-07
2026-10-14 03:52:25 LASARSAT
NORAD 62391
DTC TEST OBJECT B
NORAD 69473
4.983 11.66 1.2e-07
2026-10-14 16:53:20 LASARSAT
NORAD 62391
SL-3 DEB
NORAD 14209
4.096 7.46 2.3e-07
2026-10-16 14:20:37 ZHUHAI-1 03D
NORAD 44538
LASARSAT
NORAD 62391
3.131 14.14 2.2e-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