LEMUR-2 SONNENBLUME, 67367
Orbit data source: Space-Track
LEMUR-2 SONNENBLUME, 67367 is a payload satellite owned by Spire/Lux (US) in SSO that was launched on Sun, 11 Jan 2026 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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67367 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Com/MetRO
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
4.6 kg wet, 4.6 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.2 m
Radar Cross Section
0.054 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 LEMUR-2 SONNENBLUME
1 67367U 26004E 26206.43578503 .00002890 00000-0 31672-3 0 9993
2 67367 97.8003 204.3779 0008664 29.0043 331.1654 14.88499215 28983Epoch: 2026-07-25T10:27Z
TLE epoch observation values (Epoch: 2026-07-25T10:27:31.826Z)
Latitude
0°
Longitude
104.34719°
Altitude
600.362 km
Speed
7.562 km/s
True Right ascension
13h 37m 30s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
11:10:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
605.695 km
Perigee altitude
593.603 km
Semi-major axis
6,977.786 km
Eccentricity
0.00087
Inclination
97.8003°
RAAN
204.3779°
Arg. of periapsis
29.0043°
True anomaly
331.11747°
Mean anomaly
331.1654°
Eccentric anomaly
331.14144°
Mean motion
3.72363 °/min
Orbital period
96.68 mins
BSTAR
0.00031672
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Other satellites on launch #4 in the year 2026 (2026-01-11 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.LEMUR-2 SONNENBLUME Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-07-25 23:29:45.221Z | 141.43° SSE | 2026-07-25 23:32:45.221Z | 87.397° E | 34.253° | 2026-07-25 23:36:45.221Z | 2.486° NNE |
| 7 mins | 2026-07-26 12:50:45.221Z | 10.874° NNE | 2026-07-26 12:53:45.221Z | 306.189° NW | 44.888° | 2026-07-26 12:57:45.221Z | 195.511° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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