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 spacecraft
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
Unknown shape, 0.2 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 LEMUR-2 SONNENBLUME
1 67367U 26004E 26095.56431902 .00005488 00000-0 60403-3 0 9994
2 67367 97.7991 95.2731 0008885 32.6815 327.4949 14.87945527 12490Epoch: 2026-04-05T13:32Z
TLE epoch observation values (Epoch: 2026-04-05T13:32:37.163Z)
Latitude
-0.00009°
Longitude
58.25033°
Altitude
602.159 km
Speed
7.561 km/s
True Right ascension
06h 21m 05s
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
00:59:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
607.583 km
Perigee altitude
595.18 km
Semi-major axis
6,979.518 km
Eccentricity
0.00089
Inclination
97.7991°
RAAN
95.2731°
Arg. of periapsis
32.6815°
True anomaly
327.44014°
Mean anomaly
327.4949°
Eccentric anomaly
327.46752°
Mean motion
3.72225 °/min
Orbital period
96.72 mins
BSTAR
0.00060403
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-04-05 23:22:02.064Z | 130.519° SE | 2026-04-05 23:25:02.064Z | 68.163° E | 29.777° | 2026-04-05 23:28:02.064Z | 10.604° NNE |
| 4 mins | 2026-04-06 00:59:02.064Z | 236.039° WSW | 2026-04-06 01:01:02.064Z | 270.327° WNW | 17.051° | 2026-04-06 01:03:02.064Z | 302.476° NW |
| 7 mins | 2026-04-06 12:43:02.064Z | 17.963° NNE | 2026-04-06 12:46:02.064Z | 125.048° SE | 44.016° | 2026-04-06 12:50:02.064Z | 188.254° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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