Showing default

JACKAL-02, 59134

Orbit data source: Space-Track

JACKAL-02, 59134 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.

Loading next visibility...
Identifier
59134, 2024-043AN
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
True Anomaly
Mission
Operational Commercial Technology
Bus & Motor
JACKAL, Unknown motor
Mass
275 kg wet, 275 kg dry
Launch date (UTC)
2024-03-04 (2 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 3.0 m
Radar Cross Section
1.240 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 8 hours ago

TLE from 8 hours ago
0 JACKAL-02
1 59134U 24043AN  26133.39186544  .00011712  00000-0  25000-3 0  9992
2 59134  97.5525 277.9295 0006525 342.1829  17.9189 15.45018940122248
Epoch: 2026-05-13T09:24Z
TLE epoch observation values (Epoch: 2026-05-13T09:24:17.174Z)
Latitude
-0.00004°
Longitude
-94.29461°
Altitude
430.214 km
Speed
7.656 km/s
True Right ascension
18h 31m 43s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
01:54:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
432.703 km
Perigee altitude
423.82 km
Semi-major axis
6,806.398 km
Eccentricity
0.00065
Inclination
97.5525°
RAAN
277.9295°
Arg. of periapsis
342.1829°
True anomaly
17.94192°
Mean anomaly
17.9189°
Eccentric anomaly
17.93041°
Mean motion
3.86516 °/min
Orbital period
93.14 mins
BSTAR
0.00025
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|