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: 9 hours ago
TLE from 9 hours ago
0 HAMMER
1 59148U 24043BC 25291.27826662 .00031629 00000-0 81277-3 0 9997
2 59148 97.5226 66.1428 0007536 333.4413 26.6445 15.39204480 90461Epoch: 2025-10-18T06:40Z
TLE epoch observation values (Epoch: 2025-10-18T06:40:42.235Z)
Latitude
-0.00006°
Longitude
-61.04475°
Altitude
446.975 km
Speed
7.647 km/s
True Right ascension
04h 24m 34s
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
10:08:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
450.548 km
Perigee altitude
440.264 km
Semi-major axis
6,823.543 km
Eccentricity
0.00075
Inclination
97.5226°
RAAN
66.1428°
Arg. of periapsis
333.4413°
True anomaly
26.68326°
Mean anomaly
26.6445°
Eccentric anomaly
26.66388°
Mean motion
3.8506 °/min
Orbital period
93.49 mins
BSTAR
0.00081277
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-18 21:17:14.271Z | 43.756° NE | 2025-10-18 21:20:14.271Z | 105.972° ESE | 20.068° | 2025-10-18 21:22:14.271Z | 145.027° SSE |
| 5 mins | 2025-10-19 09:20:14.271Z | 181.709° SSW | 2025-10-19 09:22:14.271Z | 235.148° WSW | 40.72° | 2025-10-19 09:25:14.271Z | 339.071° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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