JACKAL-02, 59134
Orbit data source: Space-Track
JACKAL-02, 59134 is a payload satellite owned by True Anomaly (US) 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). Payloads include a variety of satellites, spacecraft, and rockets 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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59134 intel report (Beta)
JACKAL-02 details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 15 hours ago |
| Origin | |
| Manufacturer | True Anomaly |
| Mission | Operational Commercial Weather |
| Bus & Motor | JACKAL, Unknown motor |
| Mass | 275 kg wet, 275 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Box + 2 Pan, 1 m |
| Radar Cross Section | 0.126 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 15 hours ago
0 JACKAL-02
1 59134U 24043AN 25015.34168696 .00015207 00000-0 57243-3 0 9990
2 59134 97.4939 144.5314 0009688 257.3853 102.6303 15.27167946 48107Epoch: 2025-01-15T08:12Z
Definitive object data (Epoch: 2025-01-15T08:12:01.753Z)
| Latitude | 0.00003° |
| Longitude | -93.51132° |
| Altitude | 488.841 km |
| Speed | 7.62 km/s |
| True Right ascension | 09h 38m 07s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | -23.97732° |
| Longitude | 83.78267° |
| Altitude | 489.165 km |
| Speed | 7.622 km/s |
| Apparent Right ascension | 18h 02m 13s |
| Apparent Declination | -60° 53' 16" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 23:56:48 |
| Azimuth | 215.676° SW |
| Elevation | -33.489° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 487.889 km |
| Perigee altitude | 474.598 km |
| Semi-major axis | 6,859.38 km |
| Eccentricity | 0.0009688 |
| Inclination | 97.4939° |
| RAAN | 144.5314° |
| Arg. of periapsis | 257.3853° |
| True anomaly | 102.7386° |
| Mean anomaly | 102.6303° |
| Eccentric anomaly | 102.68445° |
| Mean motion | 3.82046 °/min |
| BSTAR | 0.00057243 |
| Orbital period | 94.23 mins |
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Other satellites on launch #43 in the year 2024 (2024-03-04 UTC)
JACKAL-02 Visibility forecast
Observer location: undefined°, undefined
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 | 2025-01-16 07:55:40.131Z | 129.12° SE | 2025-01-16 07:58:40.131Z | 60.28° ENE | 25.902° | 2025-01-16 08:00:40.131Z | 17.74° NNE |
| 5 mins | 2025-01-16 20:56:40.131Z | 36.233° NE | 2025-01-16 20:58:40.131Z | 84.939° E | 31.929° | 2025-01-16 21:01:40.131Z | 164.877° S |
Authenticating...
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