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LEMUR 2 OBA-NI-JESU, 58902

Orbit data source: Space-Track

LEMUR 2 OBA-NI-JESU, 58902 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). Payloads include a variety of satellites, spacecraft, and rockets 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	58902, 2024-022D
Orbit	SSO
Last TLE update	15 hours ago
Origin	SPIRE/NSTAR (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, 1 m
Radar Cross Section	0.146 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 15 hours ago

0 LEMUR 2 OBA-NI-JESU
1 58902U 24022D   25077.53848598  .00043923  00000-0  14251-2 0  9991
2 58902  97.4542 282.5689 0008440 277.1731  82.8550 15.31797595 62627

Epoch: 2025-03-18T12:55Z

Definitive object data (Epoch: 2025-03-18T12:55:25.188Z)

Latitude	-0.0001°
Longitude	-87.62556°
Altitude	472.84 km
Speed	7.63 km/s
True Right ascension	18h 50m 16s
True Declination	0° 00' 00"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	45.26473°
Longitude	100.53652°
Altitude	481.708 km
Speed	7.627 km/s
Apparent Right ascension	01h 42m 42s
Apparent Declination	30° 52' 25"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	08:24:25
Azimuth	300.3° NW
Elevation	12.129°
Doppler factor	1

Orbital elements

Apogee altitude	473.179 km
Perigee altitude	461.624 km
Semi-major axis	6,845.538 km
Eccentricity	0.000844
Inclination	97.4542°
RAAN	282.5689°
Arg. of periapsis	277.1731°
True anomaly	82.95098°
Mean anomaly	82.855°
Eccentric anomaly	82.90299°
Mean motion	3.83206 °/min
BSTAR	0.0014251
Orbital period	93.94 mins

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

LEMUR 2 NIMBUS2000, 58899

LEMUR 2 VALHALLA, 58900

ELECTRON KICK STAGE R/B, 58901

LEMUR 2 CAEL, 58903

ELECTRON R/B, 58904 (Decayed)

LEMUR 2 OBA-NI-JESU 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.
4 mins	2025-03-19 14:09:07.625Z	215.465° SW	2025-03-19 14:11:07.625Z	278.209° WNW	27.532°	2025-03-19 14:13:07.625Z	321.175° NNW
4 mins	2025-03-20 03:07:07.625Z	333.001° NNW	2025-03-20 03:09:07.625Z	282.796° WNW	23.725°	2025-03-20 03:11:07.625Z	238.923° WSW

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Check out LEMUR 2 OBA-NI-JESU, 58902 on other resources

View LEMUR 2 OBA-NI-JESU, 58902 on NASA - NSSDCA Website

View LEMUR 2 OBA-NI-JESU, 58902 on Heavens-Above

View LEMUR 2 OBA-NI-JESU, 58902 on Keep Track

View LEMUR 2 OBA-NI-JESU, 58902 on Celestrak

View LEMUR 2 OBA-NI-JESU, 58902 on Gunter's Space Page

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