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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 JACKAL-01
1 59127U 24043AF 26129.96174286 .00010909 00000-0 24617-3 0 9992
2 59127 97.5536 273.4854 0006672 5.7930 354.3394 15.43386027121654Epoch: 2026-05-09T23:04Z
TLE epoch observation values (Epoch: 2026-05-09T23:04:54.583Z)
Latitude
0.00007°
Longitude
59.4863°
Altitude
434.717 km
Speed
7.653 km/s
True Right ascension
18h 13m 56s
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
22:12:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
437.61 km
Perigee altitude
428.521 km
Semi-major axis
6,811.203 km
Eccentricity
0.00067
Inclination
97.5536°
RAAN
273.4854°
Arg. of periapsis
5.793°
True anomaly
354.33185°
Mean anomaly
354.3394°
Eccentric anomaly
354.33563°
Mean motion
3.86107 °/min
Orbital period
93.24 mins
BSTAR
0.00024617
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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 | 2026-05-10 22:59:47.693Z | 327.604° NNW | 2026-05-10 23:00:47.693Z | 298.354° NW | 25.792° | 2026-05-10 23:03:47.693Z | 227.516° WSW |
| 4 mins | 2026-05-11 09:27:47.693Z | 150.565° SSE | 2026-05-11 09:29:47.693Z | 31.045° NE | 39.917° | 2026-05-11 09:31:47.693Z | 356.269° 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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