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: 1 week ago
TLE from 1 week ago
0 HBTSS-SV1
1 58960U 24028F 26153.43807416 .00003564 00000-0 33122-3 0 9996
2 58960 39.9876 203.8047 0009332 93.4542 266.7316 14.95189135104978Epoch: 2026-06-02T10:30Z
TLE epoch observation values (Epoch: 2026-06-02T10:30:49.607Z)
Latitude
-0.00005°
Longitude
155.1869°
Altitude
581.612 km
Speed
7.571 km/s
True Right ascension
13h 35m 13s
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
14:33:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
590.696 km
Perigee altitude
577.702 km
Semi-major axis
6,962.336 km
Eccentricity
0.00093
Inclination
39.9876°
RAAN
203.8047°
Arg. of periapsis
93.4542°
True anomaly
266.62484°
Mean anomaly
266.7316°
Eccentric anomaly
266.67822°
Mean motion
3.73603 °/min
Orbital period
96.36 mins
BSTAR
0.00033122
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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 | 2026-06-11 04:46:55.952Z | 253.228° W | 2026-06-11 04:50:55.952Z | 160.183° S | 44.184° | 2026-06-11 04:54:55.952Z | 83.479° E |
| 6 mins | 2026-06-11 06:29:55.952Z | 274.213° WNW | 2026-06-11 06:31:55.952Z | 268.605° W | 43.791° | 2026-06-11 06:35:55.952Z | 97.118° ESE |
| 6 mins | 2026-06-11 08:10:55.952Z | 265.571° W | 2026-06-11 08:13:55.952Z | 188.409° SSW | 34.063° | 2026-06-11 08:16:55.952Z | 134.515° SE |
| 6 mins | 2026-06-12 03:10:55.952Z | 220.624° SW | 2026-06-12 03:13:55.952Z | 153.314° SSE | 33.685° | 2026-06-12 03:16:55.952Z | 91.859° ESE |
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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