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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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 26096.91419109 .00025066 00000-0 55315-3 0 9993
2 59134 97.5475 240.0462 0008428 107.0344 253.1827 15.43843407116612Epoch: 2026-04-06T21:56Z
TLE epoch observation values (Epoch: 2026-04-06T21:56:26.110Z)
Latitude
-0.00007°
Longitude
75.73899°
Altitude
439.563 km
Speed
7.647 km/s
True Right ascension
16h 00m 11s
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
13:00:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
437.458 km
Perigee altitude
425.98 km
Semi-major axis
6,809.856 km
Eccentricity
0.00084
Inclination
97.5475°
RAAN
240.0462°
Arg. of periapsis
107.0344°
True anomaly
253.09028°
Mean anomaly
253.1827°
Eccentric anomaly
253.13649°
Mean motion
3.86221 °/min
Orbital period
93.21 mins
BSTAR
0.00055315
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-04-07 08:58:31.473Z | 124.341° SE | 2026-04-07 09:00:31.473Z | 75.993° E | 24.694° | 2026-04-07 09:02:31.473Z | 22.741° NE |
| 4 mins | 2026-04-07 21:51:31.473Z | 57.491° ENE | 2026-04-07 21:52:31.473Z | 85.908° E | 24.711° | 2026-04-07 21:55:31.473Z | 157.353° SSE |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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