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LEMUR-2-SONNENBLUME

In orbit NORAD 67367 KSOI-9048-8523-1340-5541

Observations 0
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Falcon 9 Block 5 | Pandora / Twilight rideshare mission

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
LEMUR-2-SONNENBLUME
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Launch
Falcon 9 Block 5 | Pandora / Twilight rideshare mission
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
592.23 km
Apogee
605.18 km
Inclination
97.8°
Period
96.7 min
Semi-major axis
6976.8 km
Velocity
7.57 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 04:56:40 UTC
Two-line elements (TLE)
1 67367U 26004E   26283.93591659  .00002581  00000-0  28136-3 0  9998
2 67367  97.8069 280.7380 0009279 116.4855 243.7315 14.88801577 40519
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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 05:25:02 LEMUR-2-SONNENBLUME
NORAD 67367 		CZ-6A DEB
NORAD 54598 		4.718 13.99 9.7e-08
2026-10-12 06:24:59 LEMUR-2-SONNENBLUME
NORAD 67367 		SCOUT B DEB
NORAD 3392 		2.386 15.18 2.6e-07
2026-10-12 10:58:38 LEMUR-2-SONNENBLUME
NORAD 67367 		COSMOS 2251 DEB
NORAD 34729 		4.049 14.99 9.4e-08
2026-10-12 12:35:21 LEMUR-2-SONNENBLUME
NORAD 67367 		COSMOS 2251 DEB
NORAD 34729 		4.949 14.99 6.3e-08
2026-10-12 16:47:00 LEMUR-2-SONNENBLUME
NORAD 67367 		NOAA 17 DEB
NORAD 48765 		4.132 5.59 2.4e-07
2026-10-12 18:27:19 LEMUR-2-SONNENBLUME
NORAD 67367 		GRUS-3A
NORAD 69885 		3.485 11.32 2.6e-07
2026-10-13 08:00:58 LEMUR-2-SONNENBLUME
NORAD 67367 		UNKNOWN
NORAD 87164 		2.865 13.25 3.0e-07
2026-10-14 02:36:58 LEMUR-2-SONNENBLUME
NORAD 67367 		DMSP 5D-2 F11 DEB
NORAD 35534 		2.943 12.72 3.1e-07
2026-10-16 09:25:16 LEMUR-2-SONNENBLUME
NORAD 67367 		CZ-4C DEB
NORAD 37569 		4.936 14.14 8.5e-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.

All conjunctions of this satellite