JACKAL-01, 59127
Orbit data source: Space-Track
JACKAL-01, 59127 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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59127 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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 JACKAL-01
1 59127U 24043AF 25358.13126117 .00016131 00000-0 43186-3 0 9999
2 59127 97.5351 132.2792 0008823 124.0301 236.1783 15.38072375100589Epoch: 2025-12-24T03:09Z
TLE epoch observation values (Epoch: 2025-12-24T03:09:00.965Z)
Latitude
0.00004°
Longitude
-7.87988°
Altitude
458.28 km
Speed
7.636 km/s
True Right ascension
08h 49m 07s
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
09:41:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
454.781 km
Perigee altitude
442.734 km
Semi-major axis
6,826.894 km
Eccentricity
0.00088
Inclination
97.5351°
RAAN
132.2792°
Arg. of periapsis
124.0301°
True anomaly
236.09436°
Mean anomaly
236.1783°
Eccentric anomaly
236.13632°
Mean motion
3.84776 °/min
Orbital period
93.56 mins
BSTAR
0.00043186
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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-01 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 | 2025-12-24 22:26:41.038Z | 350.145° N | 2025-12-24 22:28:41.038Z | 308.383° NW | 29.294° | 2025-12-24 22:31:41.038Z | 223.173° SW |
| 5 mins | 2025-12-25 08:57:41.038Z | 146.764° SSE | 2025-12-25 08:59:41.038Z | 69.391° E | 39.721° | 2025-12-25 09:02:41.038Z | 357.421° 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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