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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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Identifier
58900, 2024-022B
Orbit
SSO
Last TLE update
16 hours ago
Origin
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Early Warn
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
~25 kg wet, ~25 kg dry
Launch date (UTC)
2024-01-31 (1 year ago)
Launch vehicle
ELECTRON
Launch site
Rocket Lab Launch Complex (RLLC)
Object type
Payload
Rocket body
Debris
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 & history

TLE from 16 hours ago
0 LEMUR 2 VALHALLA
1 58900U 24022B   25199.83942128  .00009295  00000-0  34072-3 0  9999
2 58900  97.4465  42.9692 0011058 218.3983 141.6470 15.28157901 81179
Epoch: 2025-07-18T20:08Z
TLE epoch observation values (Epoch: 2025-07-18T20:08:45.998Z)
Latitude
-0.00007°
Longitude
163.89243°
Altitude
490.372 km
Speed
7.616 km/s
True Right ascension
02h 51m 52s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
44.70055°
Longitude
157.16454°
Altitude
495.593 km
Speed
7.617 km/s
Apparent Right ascension
07h 39m 41s
Apparent Declination
20° 50' 20"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
00:53:09
Azimuth
66.726° ENE
Elevation
4.805°
Doppler factor
1
Orbital elements
Apogee altitude
485.858 km
Perigee altitude
470.694 km
Semi-major axis
6,856.413 km
Eccentricity
0.00111
Inclination
97.4465°
RAAN
42.9692°
Arg. of periapsis
218.3983°
True anomaly
141.72554°
Mean anomaly
141.647°
Eccentric anomaly
141.68628°
Mean motion
3.82294 °/min
Orbital period
94.17 mins
BSTAR
0.00034072
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