JACKAL-004, 69012
Orbit data source: Space-Track
JACKAL-004, 69012 is a payload satellite owned by True Anomaly (US) in SSO that was launched on Sun, 03 May 2026 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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69012 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
True Anomaly
Mission
Operational Commercial Imaging
Bus & Motor
JACKAL AOV, Unknown motor
Mass
275 kg wet, 275 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 14.5 m
Radar Cross Section
1.955 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 JACKAL-004
1 69012U 26100AJ 26201.83743929 .00002170 00000-0 10067-3 0 9990
2 69012 97.4605 99.2059 0004576 341.6278 18.4792 15.21108526 11923Epoch: 2026-07-20T20:05Z
TLE epoch observation values (Epoch: 2026-07-20T20:05:54.754Z)
Latitude
0.00001°
Longitude
-140.888°
Altitude
502.599 km
Speed
7.615 km/s
True Right ascension
06h 36m 49s
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
06:02:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
502.61 km
Perigee altitude
496.315 km
Semi-major axis
6,877.599 km
Eccentricity
0.00046
Inclination
97.4605°
RAAN
99.2059°
Arg. of periapsis
341.6278°
True anomaly
18.49583°
Mean anomaly
18.4792°
Eccentric anomaly
18.48751°
Mean motion
3.80529 °/min
Orbital period
94.61 mins
BSTAR
0.00010067
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Other satellites on launch #100 in the year 2026 (2026-05-03 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-004 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-07-22 05:50:03.448Z | 30.87° NE | 2026-07-22 05:52:03.448Z | 98.33° ESE | 38.942° | 2026-07-22 05:55:03.448Z | 175.866° S |
| 4 mins | 2026-07-22 16:28:03.448Z | 102.376° ESE | 2026-07-22 16:30:03.448Z | 57.49° ENE | 19.428° | 2026-07-22 16:32:03.448Z | 22.57° NE |
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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