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: 9 hours ago
TLE from 9 hours ago
0 HBTSS-SV1
1 58960U 24028F 26258.23550794 .00004869 00000-0 35902-3 0 9991
2 58960 39.9904 330.2377 0008909 117.8095 242.3603 15.03734101120701Epoch: 2026-09-15T05:39Z
TLE epoch observation values (Epoch: 2026-09-15T05:39:07.886Z)
Latitude
0.00001°
Longitude
-108.74951°
Altitude
557.712 km
Speed
7.583 km/s
True Right ascension
22h 00m 57s
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
07:10:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
563.995 km
Perigee altitude
551.637 km
Semi-major axis
6,935.953 km
Eccentricity
0.00089
Inclination
39.9904°
RAAN
330.2377°
Arg. of periapsis
117.8095°
True anomaly
242.26991°
Mean anomaly
242.3603°
Eccentric anomaly
242.3151°
Mean motion
3.75737 °/min
Orbital period
95.81 mins
BSTAR
0.00035902
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-16 07:20:22.857Z | 186.078° SSW | 2026-09-16 07:23:22.857Z | 138.419° SSE | 17.118° | 2026-09-16 07:25:22.857Z | 108.365° ESE |
| 6 mins | 2026-09-16 09:00:22.857Z | 235.045° WSW | 2026-09-16 09:03:22.857Z | 152.498° SSE | 55.834° | 2026-09-16 09:06:22.857Z | 86.971° E |
| 6 mins | 2026-09-16 10:41:22.857Z | 269.467° W | 2026-09-16 10:44:22.857Z | 79.7° E | 73.471° | 2026-09-16 10:47:22.857Z | 88.18° E |
| 6 mins | 2026-09-16 12:22:22.857Z | 271.62° WNW | 2026-09-16 12:24:22.857Z | 231.182° WSW | 59.693° | 2026-09-16 12:28:22.857Z | 115.615° SE |
| 5 mins | 2026-09-16 14:03:22.857Z | 245.454° WSW | 2026-09-16 14:05:22.857Z | 207.364° SW | 21.28° | 2026-09-16 14:08:22.857Z | 161.08° S |
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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