HBTSS-SV2, 58955
Orbit data source: Space-Track
HBTSS-SV2, 58955 is a payload satellite owned by MDA (US) in LEO that was launched on Wed, 14 Feb 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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58955 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 HBTSS-SV2
1 58955U 24028A 25259.25558362 .00000045 00000-0 13762-3 0 9998
2 58955 39.9901 222.3549 0018243 111.3087 248.9609 13.70387420 79482
TLE epoch observation values (Epoch: 2025-09-16T06:08:02.424Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #28 in the year 2024 (2024-02-14 UTC)
HBTSS-SV2 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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9 mins | 2025-09-16 23:47:00.476Z | 188.347° SSW | 2025-09-16 23:51:00.476Z | 147.374° SSE | 21.289° | 2025-09-16 23:56:00.476Z | 95.398° ESE |
11 mins | 2025-09-17 01:37:00.476Z | 233.492° WSW | 2025-09-17 01:42:00.476Z | 148.523° SSE | 41.074° | 2025-09-17 01:48:00.476Z | 80.947° E |
11 mins | 2025-09-17 03:28:00.476Z | 266.863° W | 2025-09-17 03:33:00.476Z | 78.981° E | 44.935° | 2025-09-17 03:39:00.476Z | 88.207° E |
11 mins | 2025-09-17 05:19:00.476Z | 277.415° WNW | 2025-09-17 05:24:00.476Z | 197.308° SSW | 43.657° | 2025-09-17 05:30:00.476Z | 113.907° SE |
9 mins | 2025-09-17 07:11:00.476Z | 260.523° W | 2025-09-17 07:15:00.476Z | 206.905° SW | 27.238° | 2025-09-17 07:20:00.476Z | 154.758° SSE |
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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