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: 9 hours ago
TLE from 9 hours ago
0 JACKAL-02
1 59134U 24043AN 25300.27982124 .00016966 00000-0 47343-3 0 9992
2 59134 97.5306 73.5144 0008379 330.8830 29.1945 15.36779368 91735Epoch: 2025-10-27T06:42Z
TLE epoch observation values (Epoch: 2025-10-27T06:42:56.555Z)
Latitude
-0.00006°
Longitude
-63.10517°
Altitude
453.751 km
Speed
7.643 km/s
True Right ascension
04h 54m 03s
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
11:03:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
458.313 km
Perigee altitude
446.866 km
Semi-major axis
6,830.726 km
Eccentricity
0.00084
Inclination
97.5306°
RAAN
73.5144°
Arg. of periapsis
330.883°
True anomaly
29.24138°
Mean anomaly
29.1945°
Eccentric anomaly
29.21793°
Mean motion
3.84453 °/min
Orbital period
93.64 mins
BSTAR
0.00047343
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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 | 2025-10-27 21:21:02.988Z | 40.989° NE | 2025-10-27 21:23:02.988Z | 83.709° E | 25.547° | 2025-10-27 21:26:02.988Z | 156.123° SSE |
| 5 mins | 2025-10-28 09:25:02.988Z | 196.719° SSW | 2025-10-28 09:27:02.988Z | 255.089° W | 33.812° | 2025-10-28 09:30:02.988Z | 331.59° NNW |
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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