LEMUR 2 VALHALLA, 58900
Orbit data source: Space-Track
LEMUR 2 VALHALLA, 58900 is an American payload satellite in SSO that was launched on Wed, 31 Jan 2024 UTC via an ELECTRON launch vehicle from the Rocket Lab Launch Complex (RLLC). 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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58900 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Early Warn
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
~25 kg wet, ~25 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.5 m
Radar Cross Section
0.146 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 LEMUR 2 VALHALLA
1 58900U 24022B 26075.83360846 .00014175 00000-0 39538-3 0 9999
2 58900 97.4221 284.8466 0011219 86.9287 273.3241 15.36801283118077Epoch: 2026-03-16T20:00Z
TLE epoch observation values (Epoch: 2026-03-16T20:00:23.770Z)
Latitude
-0.00003°
Longitude
170.32715°
Altitude
458.252 km
Speed
7.638 km/s
True Right ascension
18h 59m 23s
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
07:17:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
460.183 km
Perigee altitude
444.856 km
Semi-major axis
6,830.657 km
Eccentricity
0.00112
Inclination
97.4221°
RAAN
284.8466°
Arg. of periapsis
86.9287°
True anomaly
273.19575°
Mean anomaly
273.3241°
Eccentric anomaly
273.25992°
Mean motion
3.84459 °/min
Orbital period
93.64 mins
BSTAR
0.00039538
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Other satellites on launch #22 in the year 2024 (2024-01-31 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 VALHALLA 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 | 2026-03-17 02:48:54.677Z | 8.241° NNE | 2026-03-17 02:51:54.677Z | 236.594° WSW | 43.534° | 2026-03-17 02:54:54.677Z | 197.494° SSW |
| 4 mins | 2026-03-17 13:20:54.677Z | 118.7° SE | 2026-03-17 13:22:54.677Z | 64.137° ENE | 24.845° | 2026-03-17 13:24:54.677Z | 18.759° NNE |
| 4 mins | 2026-03-18 02:16:54.677Z | 51.381° ENE | 2026-03-18 02:17:54.677Z | 79.136° E | 27.357° | 2026-03-18 02:20:54.677Z | 159.158° S |
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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