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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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Identifier
58955, 2024-028A
Orbit
LEO
Country
Flag of USUS
Related 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)
2024-02-14 (2 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
1.012 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 1 week ago

TLE from 1 week ago
0 HBTSS-SV2
1 58955U 24028A   26152.26513458 -.00000009  00000-0  77002-4 0  9998
2 58955  39.9900 117.0476 0019115 150.5963 209.5863 13.70467354114881
Epoch: 2026-06-01T06:21Z
TLE epoch observation values (Epoch: 2026-06-01T06:21:47.627Z)
Latitude
0.00002°
Longitude
131.84423°
Altitude
1,009.64 km
Speed
7.342 km/s
True Right ascension
07h 48m 11s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
14:30:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,014.274 km
Perigee altitude
986.067 km
Semi-major axis
7,378.308 km
Eccentricity
0.00191
Inclination
39.99°
RAAN
117.0476°
Arg. of periapsis
150.5963°
True anomaly
209.47838°
Mean anomaly
209.5863°
Eccentric anomaly
209.53232°
Mean motion
3.42459 °/min
Orbital period
105.12 mins
BSTAR
0.000077002
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Other satellites on launch #28 in the year 2024 (2024-02-14 UTC)

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