LEMUR 2 DELOITTE-1, 63259
Orbit data source: Space-Track
LEMUR 2 DELOITTE-1, 63259 is an American payload satellite in SSO that was launched on Sat, 15 Mar 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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63259 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 DELOITTE-1
1 63259U 25052BB 26265.64868587 .00003089 00000-0 26539-3 0 9990
2 63259 97.6769 156.8760 0003105 108.9375 251.2184 14.98160401 83284TLE epoch observation values (Epoch: 2026-09-22T15:34:06.459Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #52 in the year 2025 (2025-03-15 UTC)
LEMUR 2 DELOITTE-1 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-09-23 15:46:18.050Z | 100.994° ESE | 2026-09-23 15:48:18.050Z | 71.01° E | 15.264° | 2026-09-23 15:50:18.050Z | 38.371° NE |
| 5 mins | 2026-09-23 17:21:18.050Z | 204.003° SW | 2026-09-23 17:23:18.050Z | 256.83° W | 41.007° | 2026-09-23 17:26:18.050Z | 326.722° NNW |
| 4 mins | 2026-09-24 05:02:18.050Z | 60.815° ENE | 2026-09-24 05:04:18.050Z | 107.713° ESE | 25.786° | 2026-09-24 05:06:18.050Z | 144.562° SSE |
| 4 mins | 2026-09-24 06:37:18.050Z | 323.456° NNW | 2026-09-24 06:39:18.050Z | 281.741° WNW | 22.271° | 2026-09-24 06:41:18.050Z | 247.198° WSW |
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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