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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 5 days ago
TLE from 5 days ago
0 ALICE
1 39467U 13072F 26155.32429098 .00006811 00000-0 33689-3 0 9996
2 39467 120.4611 251.3929 0161382 343.1516 16.4238 15.08625101113335Epoch: 2026-06-04T07:46Z
TLE epoch observation values (Epoch: 2026-06-04T07:46:58.740Z)
Latitude
0.00001°
Longitude
-118.12205°
Altitude
434.989 km
Speed
7.71 km/s
True Right ascension
16h 45m 34s
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
12:47:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
651.317 km
Perigee altitude
428.034 km
Semi-major axis
6,917.812 km
Eccentricity
0.01614
Inclination
120.4611°
RAAN
251.3929°
Arg. of periapsis
343.1516°
True anomaly
16.95697°
Mean anomaly
16.4238°
Eccentric anomaly
16.68934°
Mean motion
3.77216 °/min
Orbital period
95.44 mins
BSTAR
0.00033689
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-09 05:40:14.593Z | 118.869° SE | 2026-06-09 05:41:14.593Z | 89.798° E | 41.134° | 2026-06-09 05:44:14.593Z | 323.881° NNW |
| 6 mins | 2026-06-09 21:55:14.593Z | 41.496° NE | 2026-06-09 21:58:14.593Z | 234.905° WSW | 43.46° | 2026-06-09 22:01:14.593Z | 225.773° WSW |
| 4 mins | 2026-06-09 23:28:14.593Z | 352.441° N | 2026-06-09 23:29:14.593Z | 334.748° NNW | 17.264° | 2026-06-09 23:32:14.593Z | 287.345° 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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