LEMUR 2 TILLINFINITY, 63356
Orbit data source: Space-Track
LEMUR 2 TILLINFINITY, 63356 is a payload satellite owned by OroraTech (US) in SSO that was launched on Wed, 26 Mar 2025 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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63356 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 LEMUR 2 TILLINFINITY
1 63356U 25061F 26264.90248028 .00002536 00000-0 13752-3 0 9997
2 63356 97.5725 240.4362 0015997 274.1205 85.8199 15.15412837 82280TLE epoch observation values (Epoch: 2026-09-21T21:39:34.296Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #61 in the year 2025 (2025-03-26 UTC)
LEMUR 2 TILLINFINITY 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 | 2026-09-22 21:35:17.092Z | 104.351° ESE | 2026-09-22 21:37:17.092Z | 68.162° E | 18.368° | 2026-09-22 21:39:17.092Z | 31.926° NE |
| 5 mins | 2026-09-22 23:09:17.092Z | 217.179° SW | 2026-09-22 23:11:17.092Z | 265.903° W | 29.092° | 2026-09-22 23:14:17.092Z | 322.76° NNW |
| 4 mins | 2026-09-23 10:42:17.092Z | 59.375° ENE | 2026-09-23 10:44:17.092Z | 109.648° ESE | 25.786° | 2026-09-23 10:46:17.092Z | 147.474° SSE |
| 4 mins | 2026-09-23 12:16:17.092Z | 321.005° NNW | 2026-09-23 12:17:17.092Z | 301.635° NW | 19.523° | 2026-09-23 12:20:17.092Z | 246.832° 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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