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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59148 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
ES / SPNRelated business
Manufacturer
Open Cosmos
Mission
Operational Commercial Imaging
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
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 & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 HAMMER
1 59148U 24043BC 25311.48967571 .00023795 00000-0 59395-3 0 9999
2 59148 97.5251 86.9141 0007386 252.4838 107.5600 15.40152531 93573Epoch: 2025-11-07T11:45Z
TLE epoch observation values (Epoch: 2025-11-07T11:45:07.981Z)
Latitude
-0.0001°
Longitude
-136.30204°
Altitude
450.297 km
Speed
7.641 km/s
True Right ascension
05h 47m 39s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
21:04:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
447.641 km
Perigee altitude
437.565 km
Semi-major axis
6,820.74 km
Eccentricity
0.00074
Inclination
97.5251°
RAAN
86.9141°
Arg. of periapsis
252.4838°
True anomaly
107.64067°
Mean anomaly
107.56°
Eccentric anomaly
107.60034°
Mean motion
3.85297 °/min
Orbital period
93.43 mins
BSTAR
0.00059395
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Other satellites on launch #43 in the year 2024 (2024-03-04 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.HAMMER Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-11-08 09:43:55.815Z | 222.879° SW | 2025-11-08 09:44:55.815Z | 254.774° W | 27.535° | 2025-11-08 09:47:55.815Z | 325.259° NNW |
| 4 mins | 2025-11-08 22:37:55.815Z | 326.999° NNW | 2025-11-08 22:38:55.815Z | 298.542° NW | 25.399° | 2025-11-08 22:41:55.815Z | 228.652° WSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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