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
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 LEMUR-2 SONNENBLUME
1 67367U 26004E 26146.26521685 .00003133 00000-0 34563-3 0 9999
2 67367 97.7983 145.1532 0007157 204.4100 155.6779 14.88184224 20033Epoch: 2026-05-26T06:21Z
TLE epoch observation values (Epoch: 2026-05-26T06:21:54.735Z)
Latitude
-0.00002°
Longitude
165.834°
Altitude
611.2 km
Speed
7.551 km/s
True Right ascension
09h 40m 36s
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
03:34:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
605.629 km
Perigee altitude
595.64 km
Semi-major axis
6,978.771 km
Eccentricity
0.00072
Inclination
97.7983°
RAAN
145.1532°
Arg. of periapsis
204.41°
True anomaly
155.71165°
Mean anomaly
155.6779°
Eccentric anomaly
155.69478°
Mean motion
3.72284 °/min
Orbital period
96.7 mins
BSTAR
0.00034563
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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 | 2026-05-27 00:15:24.981Z | 192.148° SSW | 2026-05-27 00:17:24.981Z | 248.472° W | 39.094° | 2026-05-27 00:21:24.981Z | 337.183° NNW |
| 5 mins | 2026-05-27 12:00:24.981Z | 52.954° ENE | 2026-05-27 12:02:24.981Z | 89.772° E | 22.046° | 2026-05-27 12:05:24.981Z | 143.794° SSE |
| 5 mins | 2026-05-27 13:36:24.981Z | 331.211° NNW | 2026-05-27 13:38:24.981Z | 289.672° WNW | 24.049° | 2026-05-27 13:41:24.981Z | 237.541° WSW |
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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