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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: 7 hours ago

TLE from 7 hours ago
0 HAMMER
1 59148U 24043BC  25356.93210068  .00017899  00000-0  41600-3 0  9998
2 59148  97.5265 133.7451 0008685  94.9517 265.2722 15.42362185100575
Epoch: 2025-12-22T22:22Z
TLE epoch observation values (Epoch: 2025-12-22T22:22:13.498Z)
Latitude
Longitude
66.46575°
Altitude
442.75 km
Speed
7.646 km/s
True Right ascension
08h 54m 58s
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
04:45:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
441.999 km
Perigee altitude
430.163 km
Semi-major axis
6,814.218 km
Eccentricity
0.00087
Inclination
97.5265°
RAAN
133.7451°
Arg. of periapsis
94.9517°
True anomaly
265.17302°
Mean anomaly
265.2722°
Eccentric anomaly
265.22261°
Mean motion
3.85851 °/min
Orbital period
93.3 mins
BSTAR
0.000416
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