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: 18 hours ago
TLE from 18 hours ago
0 JACKAL-02
1 59134U 24043AN 26286.38049528 .00018896 00000-0 33814-3 0 9992
2 59134 97.5728 77.8003 0007005 133.9019 226.2812 15.50013344145903Epoch: 2026-10-13T09:07Z
TLE epoch observation values (Epoch: 2026-10-13T09:07:54.792Z)
Latitude
0.00006°
Longitude
-81.1234°
Altitude
423.105 km
Speed
7.656 km/s
True Right ascension
05h 11m 12s
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
22:04:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
418.378 km
Perigee altitude
408.863 km
Semi-major axis
6,791.757 km
Eccentricity
0.0007
Inclination
97.5728°
RAAN
77.8003°
Arg. of periapsis
133.9019°
True anomaly
226.22322°
Mean anomaly
226.2812°
Eccentric anomaly
226.25221°
Mean motion
3.87766 °/min
Orbital period
92.84 mins
BSTAR
0.00033814
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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 | 2026-10-14 10:03:13.361Z | 151.558° SSE | 2026-10-14 10:06:13.361Z | 42.669° NE | 50.259° | 2026-10-14 10:08:13.361Z | 0.136° NNE |
| 5 mins | 2026-10-14 22:53:13.361Z | 29.9° NE | 2026-10-14 22:55:13.361Z | 104.996° ESE | 51.268° | 2026-10-14 22:58:13.361Z | 177.974° S |
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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