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: 12 hours ago
TLE from 12 hours ago
0 JACKAL-01
1 59127U 24043AF 25296.92942562 .00019245 00000-0 55641-3 0 9995
2 59127 97.5310 69.5747 0008121 352.7869 7.3256 15.35643646 91186Epoch: 2025-10-23T22:18Z
TLE epoch observation values (Epoch: 2025-10-23T22:18:22.373Z)
Latitude
-0.00003°
Longitude
62.39985°
Altitude
456.609 km
Speed
7.642 km/s
True Right ascension
04h 38m 17s
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
05:02:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
461.51 km
Perigee altitude
450.41 km
Semi-major axis
6,834.097 km
Eccentricity
0.00081
Inclination
97.531°
RAAN
69.5747°
Arg. of periapsis
352.7869°
True anomaly
7.33748°
Mean anomaly
7.3256°
Eccentric anomaly
7.33154°
Mean motion
3.84168 °/min
Orbital period
93.71 mins
BSTAR
0.00055641
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-10-24 22:20:25.736Z | 333.373° NNW | 2025-10-24 22:21:25.736Z | 304.163° NW | 28.934° | 2025-10-24 22:24:25.736Z | 224.793° SW |
| 5 mins | 2025-10-25 08:51:25.736Z | 150.329° SSE | 2025-10-25 08:53:25.736Z | 53.512° ENE | 41.316° | 2025-10-25 08:56:25.736Z | 354.899° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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