SPACEMOBILE-002, 61048
Orbit data source: Space-Track
SPACEMOBILE-002, 61048 is a payload satellite owned by AST & Science (US) in LEO that was launched on Thu, 12 Sep 2024 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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61048 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 SPACEMOBILE-002
1 61048U 24163D 26259.54036756 .00017276 00000-0 79160-3 0 9994
2 61048 52.9758 249.1768 0007505 38.8059 321.3473 15.20560601111668TLE epoch observation values (Epoch: 2026-09-16T12:58:07.757Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #163 in the year 2024 (2024-09-12 UTC)
SPACEMOBILE-002 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-09-17 10:01:04.083Z | 282.91° WNW | 2026-09-17 10:04:04.083Z | 230.232° WSW | 23.216° | 2026-09-17 10:07:04.083Z | 177.63° S |
| 5 mins | 2026-09-18 01:26:04.083Z | 196.635° SSW | 2026-09-18 01:28:04.083Z | 125.3° SE | 47.999° | 2026-09-18 01:31:04.083Z | 62.538° ENE |
| 4 mins | 2026-09-18 03:05:04.083Z | 294.701° NW | 2026-09-18 03:07:04.083Z | 345.407° N | 26.253° | 2026-09-18 03:09:04.083Z | 23.8° NE |
| 6 mins | 2026-09-18 08:03:04.083Z | 327.481° NNW | 2026-09-18 08:05:04.083Z | 13.685° NNE | 44.965° | 2026-09-18 08:09:04.083Z | 109.088° ESE |
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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