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, 14.5 m
Radar Cross Section
1.240 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 JACKAL-004
1 69012U 26100AJ 26220.91460944 .00002139 00000-0 99387-4 0 9991
2 69012 97.4575 118.0993 0011819 7.6194 352.5219 15.21029662 14821Epoch: 2026-08-08T21:57Z
TLE epoch observation values (Epoch: 2026-08-08T21:57:02.255Z)
Latitude
-0.00002°
Longitude
-168.57921°
Altitude
497.759 km
Speed
7.62 km/s
True Right ascension
07h 52m 23s
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
20:09:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
507.829 km
Perigee altitude
491.571 km
Semi-major axis
6,877.837 km
Eccentricity
0.00118
Inclination
97.4575°
RAAN
118.0993°
Arg. of periapsis
7.6194°
True anomaly
352.50425°
Mean anomaly
352.5219°
Eccentric anomaly
352.51308°
Mean motion
3.80509 °/min
Orbital period
94.61 mins
BSTAR
0.000099387
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-08-09 06:23:43.631Z | 0.174° NNE | 2026-08-09 06:26:43.631Z | 310.775° NW | 35.845° | 2026-08-09 06:30:43.631Z | 210.389° SW |
| 5 mins | 2026-08-09 17:02:43.631Z | 145.078° SSE | 2026-08-09 17:04:43.631Z | 60.345° ENE | 39.999° | 2026-08-09 17:07:43.631Z | 357.468° 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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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