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 Technology
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, 2.3 m
Radar Cross Section
1.240 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 JACKAL-004
1 69012U 26100AJ 26266.29873720 .00002586 00000-0 11818-3 0 9990
2 69012 97.4524 162.9083 0012585 178.5257 181.6018 15.21406472 21725Epoch: 2026-09-23T07:10Z
TLE epoch observation values (Epoch: 2026-09-23T07:10:10.894Z)
Latitude
-0.00001°
Longitude
53.21105°
Altitude
513.345 km
Speed
7.602 km/s
True Right ascension
10h 51m 37s
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
05:22:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
507.218 km
Perigee altitude
489.909 km
Semi-major axis
6,876.7 km
Eccentricity
0.00126
Inclination
97.4524°
RAAN
162.9083°
Arg. of periapsis
178.5257°
True anomaly
181.59778°
Mean anomaly
181.6018°
Eccentric anomaly
181.59979°
Mean motion
3.80604 °/min
Orbital period
94.59 mins
BSTAR
0.00011818
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-09-23 16:46:37.398Z | 135.493° SSE | 2026-09-23 16:49:37.398Z | 63.718° ENE | 35.903° | 2026-09-23 16:52:37.398Z | 6.763° NNE |
| 5 mins | 2026-09-24 05:50:37.398Z | 27.231° NE | 2026-09-24 05:52:37.398Z | 72.21° E | 50.778° | 2026-09-24 05:55:37.398Z | 174.196° S |
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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