AEPEX, 68506
Orbit data source: Space-Track
AEPEX, 68506 is an American payload satellite in SSO that was launched on Mon, 30 Mar 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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68506 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
None
Manufacturer
Unknown
Mission
Operational spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 14.5 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 AEPEX
1 68506U 26067CU 26171.42324359 .00007011 00000-0 33724-3 0 9996
2 68506 97.4518 129.8460 0005242 80.9143 279.2685 15.19089924 12313Epoch: 2026-06-20T10:09Z
TLE epoch observation values (Epoch: 2026-06-20T10:09:28.246Z)
Latitude
0.00005°
Longitude
68.84022°
Altitude
511.098 km
Speed
7.609 km/s
True Right ascension
08h 39m 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
07:16:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.167 km
Perigee altitude
501.95 km
Semi-major axis
6,883.696 km
Eccentricity
0.00052
Inclination
97.4518°
RAAN
129.846°
Arg. of periapsis
80.9143°
True anomaly
279.20921°
Mean anomaly
279.2685°
Eccentric anomaly
279.23886°
Mean motion
3.80024 °/min
Orbital period
94.73 mins
BSTAR
0.00033724
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Other satellites on launch #67 in the year 2026 (2026-03-30 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.AEPEX 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 | 2026-06-20 21:20:36.685Z | 170.635° S | 2026-06-20 21:23:36.685Z | 193.832° SSW | 42.984° | 2026-06-20 21:27:36.685Z | 345.794° N |
| 5 mins | 2026-06-21 10:26:36.685Z | 352.791° N | 2026-06-21 10:28:36.685Z | 296.659° NW | 37.196° | 2026-06-21 10:31:36.685Z | 213.442° SW |
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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