Showing default

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.

Loading next visibility...
Identifier
59148, 2024-043BC
Orbit
SSO
Country
Flag of ESES / SPN
Related business
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 (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, 0.5 m
Radar Cross Section
0.063 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  25258.62435133  .00014441  00000-0  39456-3 0  9993
2 59148  97.5187  32.6719 0009025  89.9293 270.2985 15.37465726 85440
Epoch: 2025-09-15T14:59Z
TLE epoch observation values (Epoch: 2025-09-15T14:59:03.954Z)
Latitude
-0.0001°
Longitude
173.0791°
Altitude
456.691 km
Speed
7.639 km/s
True Right ascension
02h 10m 41s
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
13:27:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
456.717 km
Perigee altitude
444.391 km
Semi-major axis
6,828.691 km
Eccentricity
0.0009
Inclination
97.5187°
RAAN
32.6719°
Arg. of periapsis
89.9293°
True anomaly
270.19508°
Mean anomaly
270.2985°
Eccentric anomaly
270.24679°
Mean motion
3.84625 °/min
Orbital period
93.6 mins
BSTAR
0.00039456
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|