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, 0.3 m
Radar Cross Section
0.098 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 HAMMER
1 59148U 24043BC 26149.49202306 .00061485 00000-0 11126-2 0 9995
2 59148 97.5424 297.3693 0005967 244.4106 115.6529 15.49447532124917Epoch: 2026-05-29T11:48Z
TLE epoch observation values (Epoch: 2026-05-29T11:48:30.792Z)
Latitude
0.00005°
Longitude
-126.78064°
Altitude
423.225 km
Speed
7.656 km/s
True Right ascension
19h 49m 28s
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
03:55:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
419.327 km
Perigee altitude
411.22 km
Semi-major axis
6,793.411 km
Eccentricity
0.0006
Inclination
97.5424°
RAAN
297.3693°
Arg. of periapsis
244.4106°
True anomaly
115.71452°
Mean anomaly
115.6529°
Eccentric anomaly
115.68371°
Mean motion
3.87625 °/min
Orbital period
92.87 mins
BSTAR
0.0011126
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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 | 2026-05-29 23:13:39.599Z | 336.225° NNW | 2026-05-29 23:15:39.599Z | 268.33° W | 27.06° | 2026-05-29 23:17:39.599Z | 225.713° WSW |
| 4 mins | 2026-05-30 09:39:39.599Z | 135.492° SSE | 2026-05-30 09:40:39.599Z | 99.62° ESE | 36.108° | 2026-05-30 09:43:39.599Z | 1.067° NNE |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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