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). 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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59134 intel report (Beta)
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Edit Public Description
| Identifier | |
| Orbit | SSO |
| Last TLE update | 7 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, Large (>1 m²) |
Expand to show TLE details & history
TLE from 7 hours ago
0 JACKAL-02
1 59134U 24043AN 25091.79419821 .00017117 00000-0 58247-3 0 9999
2 59134 97.5014 221.5201 0009451 351.6544 8.4538 15.30453823 59781Epoch: 2025-04-01T19:03Z
Definitive object data (Epoch: 2025-04-01T19:03:38.725Z)
| Latitude | 0.00001° |
| Longitude | 105.21811° |
| Altitude | 471.152 km |
| Speed | 7.634 km/s |
| True Right ascension | 14h 46m 04s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | 55.03521° |
| Longitude | 94.69954° |
| Altitude | 480.845 km |
| Speed | 7.632 km/s |
| Apparent Right ascension | 17h 00m 38s |
| Apparent Declination | 12° 30' 20" |
| Sunlit | Object is in full shadow |
Visualization observer readout
| Local Sidereal Time | 07:16:54 |
| Azimuth | 38.601° NE |
| Elevation | -28.773° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 477.887 km |
| Perigee altitude | 464.94 km |
| Semi-major axis | 6,849.55 km |
| Eccentricity | 0.0009451 |
| Inclination | 97.5014° |
| RAAN | 221.5201° |
| Arg. of periapsis | 351.6544° |
| True anomaly | 8.46974° |
| Mean anomaly | 8.4538° |
| Eccentric anomaly | 8.46177° |
| Mean motion | 3.82869 °/min |
| BSTAR | 0.00058247 |
| Orbital period | 94.03 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-04-02 07:45:44.593Z | 112.475° ESE | 2025-04-02 07:47:44.593Z | 76.917° E | 17.081° | 2025-04-02 07:49:44.593Z | 35.23° NE |
| 4 mins | 2025-04-02 09:19:44.593Z | 229.02° WSW | 2025-04-02 09:20:44.593Z | 252.528° W | 21.236° | 2025-04-02 09:23:44.593Z | 316.346° NNW |
Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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