LILACSAT 2
In orbit NORAD 40908 AHVS-7983-8710-8819-8034 China
Time in UTC
18:53
Next pass · ИТ-куб, Калининград
—
No observations scheduled
18
Observations over 30 days
47%
Successful observations
33k
Frames, latest 2026-10-10 17:27 UTC
The satellite is in orbit
Gallery
1 40908U 15049K 26283.26632742 .00020905 00000-0 31206-3 0 9994
2 40908 97.4520 324.7043 0006497 174.4109 185.7218 15.55059416613615
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.
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 11:33:58 |
LILACSAT-2
NORAD 40908 |
OBJECT AU
NORAD 61777 |
4.586 | 15.11 | 7.7e-08 |
| 2026-10-12 20:23:29 |
LILACSAT-2
NORAD 40908 |
STARLINK-32678
NORAD 62309 |
1.016 | 10.91 | 9.6e-05 |
| 2026-10-13 19:42:26 |
LILACSAT-2
NORAD 40908 |
SHARJAHSAT-1
NORAD 55104 |
3.067 | 3.82 | 4.6e-07 |
| 2026-10-16 00:14:51 |
LILACSAT-2
NORAD 40908 |
COSMOS 1508
NORAD 14483 |
4.651 | 15.58 | 6.8e-08 |
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.
