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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Edit Public Description
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: 17 hours ago
TLE from 17 hours ago
0 HBTSS-SV1
1 58960U 24028F 25259.10688787 .00000417 00000-0 17793-3 0 9994
2 58960 39.9884 164.8506 0010339 179.8767 180.2007 14.34599314 66836Epoch: 2025-09-16T02:33Z
TLE epoch observation values (Epoch: 2025-09-16T02:33:55.111Z)
Latitude
-0°
Longitude
131.06903°
Altitude
783.259 km
Speed
7.46 km/s
True Right ascension
10h 59m 24s
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
12:40:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
786.145 km
Perigee altitude
771.346 km
Semi-major axis
7,156.883 km
Eccentricity
0.00103
Inclination
39.9884°
RAAN
164.8506°
Arg. of periapsis
179.8767°
True anomaly
180.20029°
Mean anomaly
180.2007°
Eccentric anomaly
180.20049°
Mean motion
3.58474 °/min
Orbital period
100.43 mins
BSTAR
0.00017793
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-09-16 21:08:58.953Z | 217.059° SW | 2025-09-16 21:12:58.953Z | 159.009° S | 32.459° | 2025-09-16 21:17:58.953Z | 86.445° E |
| 9 mins | 2025-09-16 22:54:58.953Z | 256.041° W | 2025-09-16 22:58:58.953Z | 144.142° SSE | 44.713° | 2025-09-16 23:03:58.953Z | 83.421° E |
| 9 mins | 2025-09-17 00:40:58.953Z | 275.468° WNW | 2025-09-17 00:44:58.953Z | 146.299° SSE | 44.834° | 2025-09-17 00:49:58.953Z | 100.641° ESE |
| 8 mins | 2025-09-17 02:26:58.953Z | 268.425° W | 2025-09-17 02:30:58.953Z | 192.494° SSW | 34.096° | 2025-09-17 02:34:58.953Z | 137.767° 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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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