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: 10 hours ago
TLE from 10 hours ago
0 JACKAL-02
1 59134U 24043AN 26251.37649874 .00021776 00000-0 40568-3 0 9998
2 59134 97.5672 41.0769 0005559 266.6328 93.4287 15.48842747140484Epoch: 2026-09-08T09:02Z
TLE epoch observation values (Epoch: 2026-09-08T09:02:09.491Z)
Latitude
0.00006°
Longitude
-81.90645°
Altitude
423.463 km
Speed
7.657 km/s
True Right ascension
02h 44m 18s
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
11:30:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
420.822 km
Perigee altitude
413.267 km
Semi-major axis
6,795.182 km
Eccentricity
0.00056
Inclination
97.5672°
RAAN
41.0769°
Arg. of periapsis
266.6328°
True anomaly
93.49228°
Mean anomaly
93.4287°
Eccentric anomaly
93.46049°
Mean motion
3.87473 °/min
Orbital period
92.91 mins
BSTAR
0.00040568
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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 | 2026-09-08 23:33:29.352Z | 332.535° NNW | 2026-09-08 23:35:29.352Z | 275.247° WNW | 25.874° | 2026-09-08 23:37:29.352Z | 233.039° WSW |
| 4 mins | 2026-09-09 09:59:29.352Z | 151.453° SSE | 2026-09-09 10:01:29.352Z | 36.753° NE | 59.164° | 2026-09-09 10:03:29.352Z | 356.493° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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