HBTSS-SV1, 58960
Orbit data source: Space-Track
HBTSS-SV1, 58960 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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58960 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
L3Harris SIS
Mission
Operational Commercial Early Warn
Bus & Motor
HBT-L3H, 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: 15 hours ago
TLE from 15 hours ago
0 HBTSS-SV1
1 58960U 24028F 26077.91728917 .00001965 00000-0 24549-3 0 9998
2 58960 39.9858 266.6812 0011733 286.2871 73.6625 14.84292151 93695Epoch: 2026-03-18T22:00Z
TLE epoch observation values (Epoch: 2026-03-18T22:00:53.784Z)
Latitude
-0.00004°
Longitude
119.98287°
Altitude
612.962 km
Speed
7.556 km/s
True Right ascension
17h 46m 43s
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
17:57:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
626.419 km
Perigee altitude
610.001 km
Semi-major axis
6,996.347 km
Eccentricity
0.00117
Inclination
39.9858°
RAAN
266.6812°
Arg. of periapsis
286.2871°
True anomaly
73.79157°
Mean anomaly
73.6625°
Eccentric anomaly
73.72703°
Mean motion
3.70882 °/min
Orbital period
97.07 mins
BSTAR
0.00024549
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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-SV1 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-03-19 15:58:50.791Z | 220.624° SW | 2026-03-19 16:02:50.791Z | 158.436° S | 30.676° | 2026-03-19 16:06:50.791Z | 89.458° E |
| 7 mins | 2026-03-19 17:41:50.791Z | 256.8° W | 2026-03-19 17:44:50.791Z | 202.131° SSW | 44.662° | 2026-03-19 17:48:50.791Z | 84.143° E |
| 7 mins | 2026-03-19 19:23:50.791Z | 275.307° WNW | 2026-03-19 19:26:50.791Z | 256.608° W | 43.965° | 2026-03-19 19:30:50.791Z | 101.145° ESE |
| 6 mins | 2026-03-19 21:06:50.791Z | 259.468° W | 2026-03-19 21:08:50.791Z | 217.562° SW | 31.656° | 2026-03-19 21:12:50.791Z | 139.911° SSE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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