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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Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 LEMUR 2 OBA-NI-JESU
1 58902U 24022D 25259.08111590 .00033775 00000-0 79200-3 0 9998
2 58902 97.4342 106.4539 0006705 358.2631 1.8591 15.41977831 90514
TLE epoch observation values (Epoch: 2025-09-16T01:56:48.413Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #22 in the year 2024 (2024-01-31 UTC)
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. |
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4 mins | 2025-09-17 03:26:01.569Z | 330.612° NNW | 2025-09-17 03:28:01.569Z | 276.558° WNW | 22.765° | 2025-09-17 03:30:01.569Z | 235.508° WSW |
4 mins | 2025-09-17 13:55:01.569Z | 159.348° S | 2025-09-17 13:56:01.569Z | 144.655° SSE | 41.422° | 2025-09-17 13:59:01.569Z | 351.537° N |
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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