CINEMA 2, 39424
Orbit data source: Space-Track
CINEMA 2, 39424 is a payload satellite owned by Kyung Hee U (US) in SSO that was launched on Thu, 21 Nov 2013 UTC via a DNEPR launch vehicle from the Orenburg, Russia (OREN). 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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39424 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
KHUS/UCB
Mission
Non-operational Amateur Science
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 + 1 Rod, 0.3 m
Radar Cross Section
0.035 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 CINEMA 2
1 39424U 13066J 26092.27514736 .00004691 00000-0 53979-3 0 9998
2 39424 97.8834 24.0798 0076121 18.8993 341.5019 14.84147278664834Epoch: 2026-04-02T06:36Z
TLE epoch observation values (Epoch: 2026-04-02T06:36:12.731Z)
Latitude
-0.00006°
Longitude
94.40079°
Altitude
568.831 km
Speed
7.604 km/s
True Right ascension
01h 36m 19s
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
21:47:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
666.518 km
Perigee altitude
560.079 km
Semi-major axis
6,991.435 km
Eccentricity
0.00761
Inclination
97.8834°
RAAN
24.0798°
Arg. of periapsis
18.8993°
True anomaly
341.22263°
Mean anomaly
341.5019°
Eccentric anomaly
341.36252°
Mean motion
3.71273 °/min
Orbital period
96.96 mins
BSTAR
0.00053979
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Other satellites on launch #66 in the year 2013 (2013-11-21 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.CINEMA 2 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 | 2026-04-02 19:41:25.524Z | 190.418° SSW | 2026-04-02 19:43:25.524Z | 260.355° W | 40.053° | 2026-04-02 19:46:25.524Z | 335.456° NNW |
| 5 mins | 2026-04-03 07:28:25.524Z | 59.715° ENE | 2026-04-03 07:30:25.524Z | 99.021° ESE | 22.859° | 2026-04-03 07:33:25.524Z | 146.719° SSE |
| 5 mins | 2026-04-03 09:04:25.524Z | 329.115° NNW | 2026-04-03 09:06:25.524Z | 285.581° WNW | 25.701° | 2026-04-03 09:09:25.524Z | 235.842° WSW |
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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