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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
Last TLE update
8 hours ago
Origin
Manufacturer
Open Cosmos
Mission
Operational Commercial Com/MetRO
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
2024-03-04 (1 year ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 0.5 m
Radar Cross Section
0.063 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 8 hours ago
0 HAMMER
1 59148U 24043BC  25199.62108561  .00008569  00000-0  24931-3 0  9995
2 59148  97.5122 332.4084 0007112 301.8623  58.1928 15.35663349 76385
Epoch: 2025-07-18T14:54Z
TLE epoch observation values (Epoch: 2025-07-18T14:54:21.796Z)
Latitude
-0°
Longitude
172.14766°
Altitude
459.498 km
Speed
7.638 km/s
True Right ascension
22h 09m 38s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
48.56983°
Longitude
1.04933°
Altitude
471.414 km
Speed
7.632 km/s
Apparent Right ascension
04h 36m 37s
Apparent Declination
31° 51' 18"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
12:05:13
Azimuth
307.803° NW
Elevation
5.338°
Doppler factor
1
Orbital elements
Apogee altitude
460.761 km
Perigee altitude
451.04 km
Semi-major axis
6,834.037 km
Eccentricity
0.00071
Inclination
97.5122°
RAAN
332.4084°
Arg. of periapsis
301.8623°
True anomaly
58.26209°
Mean anomaly
58.1928°
Eccentric anomaly
58.22744°
Mean motion
3.84173 °/min
Orbital period
93.71 mins
BSTAR
0.00024931
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