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

LILIUM-2

In orbit NORAD 66679 TBRA-6788-0701-0482-9659

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

7

Observations all time

Mission information
Spacecraft name
LILIUM-2
Other names
NCKU-LILIUM-2
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
2025-11-28 18:44:30
Separation time
2025-11-28 19:40:12
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
504.08 km
Apogee
510.69 km
Inclination
97.4°
Period
94.8 min
Semi-major axis
6885.5 km
Velocity
7.61 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 14:09:04 UTC
Two-line elements (TLE)
1 66679U 25276P   26287.13842622  .00003175  00000-0  15725-3 0  9998
2 66679 97.4039 357.7595 0004802 324.7056 35.3859 15.18485649 48444
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 15:36:41 LILIUM-2
NORAD 66679
SNAPPY
NORAD 69014
4.897 15.07 6.6e-08
2026-10-15 19:13:45 SCS-01 A
NORAD 63982
LILIUM-2
NORAD 66679
3.625 0.07 3.3e-07
2026-10-16 06:05:03 STARLINK-30223
NORAD 57603
LILIUM-2
NORAD 66679
3.398 8.92 9.6e-06
2026-10-17 01:19:40 DTUSAT-2
NORAD 40030
LILIUM-2
NORAD 66679
3.801 8.09 2.6e-07
2026-10-17 21:05:50 LILIUM-2
NORAD 66679
CONNECTA IOT-16
NORAD 67390
3.749 8.98 2.6e-07
2026-10-17 21:53:16 LILIUM-2
NORAD 66679
CONNECTA IOT-16
NORAD 67390
2.907 9.00 4.3e-07
2026-10-18 15:15:49 PRSC-EO1
NORAD 62725
LILIUM-2
NORAD 66679
0.372 0.08 3.2e-05
2026-10-19 05:26:24 LILIUM-2
NORAD 66679
CZ-4B R/B
NORAD 33410
2.113 0.24 9.9e-07
2026-10-20 07:49:54 LILIUM-2
NORAD 66679
ELECTRON KICK STAGE R/B
NORAD 58579
1.913 9.07 1.0e-06
2026-10-20 21:49:14 LILIUM-2
NORAD 66679
TRANSPORTER-15 OBJECT AA
NORAD 66690
3.593 0.08 3.4e-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