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
Country
USRelated business
Manufacturer
True Anomaly
Mission
Operational Commercial Technology
Bus & Motor
JACKAL, Unknown motor
Mass
275 kg wet, 275 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 3.0 m
Radar Cross Section
1.240 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 JACKAL-02
1 59134U 24043AN 25312.84443826 .00024468 00000-0 66929-3 0 9996
2 59134 97.5322 86.3866 0007888 281.5542 78.4816 15.37325901 93661Epoch: 2025-11-08T20:15Z
TLE epoch observation values (Epoch: 2025-11-08T20:15:59.465Z)
Latitude
-0.00007°
Longitude
94.12062°
Altitude
456.058 km
Speed
7.64 km/s
True Right ascension
05h 45m 32s
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
11:41:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
456.356 km
Perigee altitude
445.582 km
Semi-major axis
6,829.106 km
Eccentricity
0.00079
Inclination
97.5322°
RAAN
86.3866°
Arg. of periapsis
281.5542°
True anomaly
78.57019°
Mean anomaly
78.4816°
Eccentric anomaly
78.52589°
Mean motion
3.84589 °/min
Orbital period
93.61 mins
BSTAR
0.00066929
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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.JACKAL-02 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 | 2025-11-10 21:15:36.521Z | 42.884° NE | 2025-11-10 21:18:36.521Z | 107.338° ESE | 21.281° | 2025-11-10 21:20:36.521Z | 147.052° SSE |
| 5 mins | 2025-11-11 09:19:36.521Z | 187.33° SSW | 2025-11-11 09:21:36.521Z | 256.896° W | 39.525° | 2025-11-11 09:24:36.521Z | 337.504° N |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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