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). 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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58902 intel report (Beta)
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Edit Public Description
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: 1 day ago
TLE from 1 day ago
0 LEMUR 2 OBA-NI-JESU
1 58902U 24022D 25255.83620107 .00021112 00000-0 49974-3 0 9993
2 58902 97.4341 103.1477 0007032 9.9704 350.1681 15.41788000 90016Epoch: 2025-09-12T20:04Z
TLE epoch observation values (Epoch: 2025-09-12T20:04:07.772Z)
Latitude
-0.00003°
Longitude
170.03712°
Altitude
439.226 km
Speed
7.651 km/s
True Right ascension
06h 52m 35s
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
17:27:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
442.563 km
Perigee altitude
432.977 km
Semi-major axis
6,815.907 km
Eccentricity
0.0007
Inclination
97.4341°
RAAN
103.1477°
Arg. of periapsis
9.9704°
True anomaly
350.15433°
Mean anomaly
350.1681°
Eccentric anomaly
350.16122°
Mean motion
3.85707 °/min
Orbital period
93.34 mins
BSTAR
0.00049974
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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 OBA-NI-JESU 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-09-14 02:13:52.663Z | 40.687° NE | 2025-09-14 02:15:52.663Z | 82.31° E | 24.367° | 2025-09-14 02:18:52.663Z | 155.058° SSE |
| 5 mins | 2025-09-14 14:15:52.663Z | 195.256° SSW | 2025-09-14 14:17:52.663Z | 271.454° WNW | 35.823° | 2025-09-14 14:20:52.663Z | 335.786° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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