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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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
NGIS
Mission
Operational Commercial Early Warn
Bus & Motor
HBT-NG, Unknown motor
Mass
~1,000 kg wet, ~1,000 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
1.012 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 HBTSS-SV2
1 58955U 24028A 25352.54888426 -.00000021 00000-0 63463-4 0 9990
2 58955 39.9890 153.7799 0020395 284.1261 75.7219 13.70421385 92282Epoch: 2025-12-18T13:10Z
TLE epoch observation values (Epoch: 2025-12-18T13:10:23.600Z)
Latitude
-0.00002°
Longitude
-131.22125°
Altitude
993.859 km
Speed
7.358 km/s
True Right ascension
10h 15m 07s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
22:42:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,015.384 km
Perigee altitude
985.287 km
Semi-major axis
7,378.473 km
Eccentricity
0.00204
Inclination
39.989°
RAAN
153.7799°
Arg. of periapsis
284.1261°
True anomaly
75.94853°
Mean anomaly
75.7219°
Eccentric anomaly
75.8352°
Mean motion
3.42447 °/min
Orbital period
105.13 mins
BSTAR
0.000063463
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Other satellites on launch #28 in the year 2024 (2024-02-14 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2025-12-19 13:51:03.321Z | 211.607° SW | 2025-12-19 13:56:03.321Z | 149.199° SSE | 32.255° | 2025-12-19 14:02:03.321Z | 84.17° E |
| 11 mins | 2025-12-19 15:42:03.321Z | 251.866° W | 2025-12-19 15:47:03.321Z | 137.793° SSE | 44.452° | 2025-12-19 15:53:03.321Z | 82.139° E |
| 11 mins | 2025-12-19 17:33:03.321Z | 274.813° WNW | 2025-12-19 17:38:03.321Z | 198.113° SSW | 44.983° | 2025-12-19 17:44:03.321Z | 98.262° ESE |
| 11 mins | 2025-12-19 19:24:03.321Z | 274.828° WNW | 2025-12-19 19:29:03.321Z | 205.642° SW | 38.405° | 2025-12-19 19:35:03.321Z | 131.603° SE |
| 6 mins | 2025-12-19 21:17:03.321Z | 244.45° WSW | 2025-12-19 21:19:03.321Z | 223.63° SW | 17.129° | 2025-12-19 21:23:03.321Z | 184.099° SSW |
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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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