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 spacecraft
Bus & Motor
JACKAL AOV, Unknown motor
Mass
275 kg wet, 275 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 14.5 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 JACKAL-004
1 69012U 26100AJ 26175.51902499 .00003718 00000-0 17200-3 0 9999
2 69012 97.3993 73.2275 0007796 25.1581 335.0033 15.20731326 7922Epoch: 2026-06-24T12:27Z
TLE epoch observation values (Epoch: 2026-06-24T12:27:23.759Z)
Latitude
0.00001°
Longitude
-26.29657°
Altitude
501.862 km
Speed
7.616 km/s
True Right ascension
04h 52m 54s
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
05:52:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
505.961 km
Perigee altitude
495.235 km
Semi-major axis
6,878.735 km
Eccentricity
0.00078
Inclination
97.3993°
RAAN
73.2275°
Arg. of periapsis
25.1581°
True anomaly
334.96552°
Mean anomaly
335.0033°
Eccentric anomaly
334.98441°
Mean motion
3.80435 °/min
Orbital period
94.63 mins
BSTAR
0.000172
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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 | 2026-06-25 06:23:33.011Z | 355.826° N | 2026-06-25 06:26:33.011Z | 261.169° W | 36.109° | 2026-06-25 06:29:33.011Z | 210.647° SW |
| 5 mins | 2026-06-25 17:01:33.011Z | 146.863° SSE | 2026-06-25 17:03:33.011Z | 83.766° E | 39.892° | 2026-06-25 17:06:33.011Z | 359.034° 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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