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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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Iframe URL

https://www.satcat.com/sats-embedded/58900?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

58900, 2024-022B

Orbit

SSO

Last TLE update

16 hours ago

Origin

Spire Global (US)

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

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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Other satellites on launch #22 in the year 2024 (2024-01-31 UTC)

LEMUR 2 NIMBUS2000, 58899

ELECTRON KICK STAGE R/B, 58901

LEMUR 2 OBA-NI-JESU, 58902

LEMUR 2 CAEL, 58903

ELECTRON R/B, 58904 (Decayed)

LEMUR 2 VALHALLA Visibility forecast

Observer location: undefined°, undefined°

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	2025-07-19 13:33:28.918Z	163.576° S	2025-07-19 13:36:28.918Z	102.925° ESE	44.607°	2025-07-19 13:39:28.918Z	350.529° N
5 mins	2025-07-20 02:34:28.918Z	5.09° NNE	2025-07-20 02:36:28.918Z	328.72° NNW	42.22°	2025-07-20 02:39:28.918Z	201.166° 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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Authenticating...

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Check out LEMUR 2 VALHALLA, 58900 on other resources

View LEMUR 2 VALHALLA, 58900 on NASA - NSSDCA Website

View LEMUR 2 VALHALLA, 58900 on Heavens-Above

View LEMUR 2 VALHALLA, 58900 on Keep Track

View LEMUR 2 VALHALLA, 58900 on Celestrak

View LEMUR 2 VALHALLA, 58900 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.