ALICE, 39467
Orbit data source: Space-Track
ALICE, 39467 is a payload satellite owned by AFIT (US) in LEO that was launched on Fri, 06 Dec 2013 UTC via an ATLAS V 501 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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39467 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
AFIT
Mission
Operational Defense Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
4 kg wet, 4 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 4 Pan, 0.3 m
Radar Cross Section
0.066 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 ALICE
1 39467U 13072F 26094.66834067 .00014798 00000-0 73910-3 0 9995
2 39467 120.4609 20.9739 0156581 275.8828 82.4411 15.07757100104186Epoch: 2026-04-04T16:02Z
TLE epoch observation values (Epoch: 2026-04-04T16:02:24.633Z)
Latitude
-0.00011°
Longitude
-52.61349°
Altitude
532.014 km
Speed
7.605 km/s
True Right ascension
01h 23m 53s
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
19:26:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
650.692 km
Perigee altitude
433.969 km
Semi-major axis
6,920.468 km
Eccentricity
0.01566
Inclination
120.4609°
RAAN
20.9739°
Arg. of periapsis
275.8828°
True anomaly
84.2241°
Mean anomaly
82.4411°
Eccentric anomaly
83.33217°
Mean motion
3.76999 °/min
Orbital period
95.49 mins
BSTAR
0.0007391
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Other satellites on launch #72 in the year 2013 (2013-12-06 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.ALICE 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 | 2026-04-05 16:08:42.105Z | 71.684° E | 2026-04-05 16:11:42.105Z | 24.595° NE | 17.672° | 2026-04-05 16:13:42.105Z | 353.428° N |
| 6 mins | 2026-04-05 17:40:42.105Z | 132.378° SE | 2026-04-05 17:42:42.105Z | 119.022° SE | 43.183° | 2026-04-05 17:46:42.105Z | 318.754° NNW |
| 6 mins | 2026-04-06 09:57:42.105Z | 36.246° NE | 2026-04-06 10:00:42.105Z | 274.479° WNW | 42.965° | 2026-04-06 10:03:42.105Z | 232.346° WSW |
| 4 mins | 2026-04-06 11:30:42.105Z | 353.332° N | 2026-04-06 11:31:42.105Z | 336.966° NNW | 16.671° | 2026-04-06 11:34:42.105Z | 291.676° WNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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