LEMUR-2 MARIO-SOUSA, 67365
Orbit data source: Space-Track
LEMUR-2 MARIO-SOUSA, 67365 is a payload satellite owned by Spire/Lux (US) in SSO that was launched on Sun, 11 Jan 2026 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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67365 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 LEMUR-2 MARIO-SOUSA
1 67365U 26004C 26146.53816729 .00004769 00000-0 52117-3 0 9994
2 67365 97.7988 145.4298 0007538 200.8484 159.2427 14.88309484 20077TLE epoch observation values (Epoch: 2026-05-26T12:54:57.653Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #4 in the year 2026 (2026-01-11 UTC)
LEMUR-2 MARIO-SOUSA 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 | 2026-05-26 22:46:09.020Z | 91.563° ESE | 2026-05-26 22:48:09.020Z | 60.682° ENE | 14.374° | 2026-05-26 22:50:09.020Z | 31.942° NE |
| 6 mins | 2026-05-27 00:21:09.020Z | 200.001° SSW | 2026-05-27 00:23:09.020Z | 255.691° W | 36.079° | 2026-05-27 00:27:09.020Z | 334.495° NNW |
| 5 mins | 2026-05-27 12:06:09.020Z | 51.976° ENE | 2026-05-27 12:08:09.020Z | 93.013° ESE | 24.785° | 2026-05-27 12:11:09.020Z | 149.295° SSE |
| 5 mins | 2026-05-27 13:42:09.020Z | 326.168° NNW | 2026-05-27 13:44:09.020Z | 286.214° WNW | 21.463° | 2026-05-27 13:47:09.020Z | 239.661° 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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