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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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: 2 days ago
TLE from 2 days ago
0 JACKAL-01
1 59127U 24043AF 26308.41180159 .00014905 00000-0 28007-3 0 9994
2 59127 97.5741 99.5878 0007222 73.3817 286.8225 15.48668399149227Epoch: 2026-11-04T09:52Z
TLE epoch observation values (Epoch: 2026-11-04T09:52:59.657Z)
Latitude
-0.00008°
Longitude
-92.32125°
Altitude
422.327 km
Speed
7.659 km/s
True Right ascension
06h 38m 21s
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
12:08:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
422.463 km
Perigee altitude
412.648 km
Semi-major axis
6,795.693 km
Eccentricity
0.00072
Inclination
97.5741°
RAAN
99.5878°
Arg. of periapsis
73.3817°
True anomaly
286.74326°
Mean anomaly
286.8225°
Eccentric anomaly
286.78288°
Mean motion
3.87429 °/min
Orbital period
92.92 mins
BSTAR
0.00028007
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-11-06 22:54:36.319Z | 20.76° NNE | 2026-11-06 22:57:36.319Z | 84.276° E | 55.076° | 2026-11-06 23:00:36.319Z | 179.14° S |
| 4 mins | 2026-11-07 10:54:36.319Z | 225.241° WSW | 2026-11-07 10:55:36.319Z | 251.337° W | 23.73° | 2026-11-07 10:58:36.319Z | 319.723° NNW |
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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