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: 8 hours ago
TLE from 8 hours ago
0 JACKAL-01
1 59127U 24043AF 25346.93999190 .00022631 00000-0 61104-3 0 9995
2 59127 97.5336 120.7928 0008220 161.3436 198.8111 15.37743184 98867Epoch: 2025-12-12T22:33Z
TLE epoch observation values (Epoch: 2025-12-12T22:33:35.300Z)
Latitude
-0.00003°
Longitude
60.52131°
Altitude
461.212 km
Speed
7.633 km/s
True Right ascension
08h 03m 10s
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
05:26:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
455.345 km
Perigee altitude
444.12 km
Semi-major axis
6,827.869 km
Eccentricity
0.00082
Inclination
97.5336°
RAAN
120.7928°
Arg. of periapsis
161.3436°
True anomaly
198.78076°
Mean anomaly
198.8111°
Eccentric anomaly
198.79593°
Mean motion
3.84694 °/min
Orbital period
93.58 mins
BSTAR
0.00061104
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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 | 2025-12-13 09:37:55.328Z | 209.585° SW | 2025-12-13 09:39:55.328Z | 269.505° W | 28.424° | 2025-12-13 09:41:55.328Z | 319.488° NNW |
| 4 mins | 2025-12-13 22:33:55.328Z | 322.225° NNW | 2025-12-13 22:34:55.328Z | 291.292° WNW | 25.666° | 2025-12-13 22:37:55.328Z | 226.919° WSW |
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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