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HAMMER, 59148

Orbit data source: Space-Track

HAMMER, 59148 is a payload satellite owned by Open Cosmos (ES) in SSO that was launched on Mon, 04 Mar 2024 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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
59148, 2024-043BC
Orbit
SSO
Country
Flag of ESES / SPN
Related business
Manufacturer
Open Cosmos
Mission
Operational Commercial Imaging
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
2024-03-04 (2 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 0.3 m
Radar Cross Section
0.098 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 6 hours ago

TLE from 6 hours ago
0 HAMMER
1 59148U 24043BC  26096.93999086  .00024355  00000-0  48053-3 0  9998
2 59148  97.5374 242.5656 0007801  80.3784 279.8346 15.47145063116788
Epoch: 2026-04-06T22:33Z
TLE epoch observation values (Epoch: 2026-04-06T22:33:35.210Z)
Latitude
-0.00006°
Longitude
68.94504°
Altitude
427.303 km
Speed
7.656 km/s
True Right ascension
16h 10m 15s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
10:55:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
427.323 km
Perigee altitude
416.713 km
Semi-major axis
6,800.155 km
Eccentricity
0.00078
Inclination
97.5374°
RAAN
242.5656°
Arg. of periapsis
80.3784°
True anomaly
279.74651°
Mean anomaly
279.8346°
Eccentric anomaly
279.79055°
Mean motion
3.87048 °/min
Orbital period
93.01 mins
BSTAR
0.00048053
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