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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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, 1.0 m
Radar Cross Section
0.098 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 HAMMER
1 59148U 24043BC 26220.44311352 .00013539 00000-0 20289-3 0 9990
2 59148 97.5473 11.9259 0003686 31.4565 328.6908 15.55070564135922Epoch: 2026-08-08T10:38Z
TLE epoch observation values (Epoch: 2026-08-08T10:38:05.008Z)
Latitude
-0.00005°
Longitude
-104.54935°
Altitude
402.946 km
Speed
7.67 km/s
True Right ascension
00h 47m 42s
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
15:35:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
401.371 km
Perigee altitude
396.375 km
Semi-major axis
6,777.01 km
Eccentricity
0.00037
Inclination
97.5473°
RAAN
11.9259°
Arg. of periapsis
31.4565°
True anomaly
328.66884°
Mean anomaly
328.6908°
Eccentric anomaly
328.67982°
Mean motion
3.89033 °/min
Orbital period
92.54 mins
BSTAR
0.00020289
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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 | 2026-08-10 10:38:09.094Z | 196.861° SSW | 2026-08-10 10:40:09.094Z | 239.458° WSW | 27.623° | 2026-08-10 10:43:09.094Z | 326.095° NNW |
| 4 mins | 2026-08-10 23:26:09.094Z | 337.765° N | 2026-08-10 23:27:09.094Z | 301.524° NW | 31.962° | 2026-08-10 23:30:09.094Z | 216.396° SW |
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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