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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Edit Public Description
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: 8 hours ago
TLE from 8 hours ago
0 CINEMA 2
1 39424U 13066J 25300.53471341 .00002991 00000-0 35590-3 0 9992
2 39424 97.8693 229.4373 0077237 168.3037 191.9994 14.83008121641595Epoch: 2025-10-27T12:49Z
TLE epoch observation values (Epoch: 2025-10-27T12:49:59.238Z)
Latitude
-0.00006°
Longitude
0.80531°
Altitude
675.77 km
Speed
7.49 km/s
True Right ascension
15h 17m 44s
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
15:53:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
670.908 km
Perigee altitude
562.853 km
Semi-major axis
6,995.017 km
Eccentricity
0.00772
Inclination
97.8693°
RAAN
229.4373°
Arg. of periapsis
168.3037°
True anomaly
191.81711°
Mean anomaly
191.9994°
Eccentric anomaly
191.90809°
Mean motion
3.70988 °/min
Orbital period
97.04 mins
BSTAR
0.0003559
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-10-28 07:14:56.427Z | 61.066° ENE | 2025-10-28 07:16:56.427Z | 93.807° ESE | 15.422° | 2025-10-28 07:18:56.427Z | 126.236° SE |
| 5 mins | 2025-10-28 08:50:56.427Z | 342.037° N | 2025-10-28 08:52:56.427Z | 295.648° NW | 30.005° | 2025-10-28 08:55:56.427Z | 228.575° WSW |
| 7 mins | 2025-10-28 19:43:56.427Z | 188.566° SSW | 2025-10-28 19:46:56.427Z | 267° W | 39.004° | 2025-10-28 19:50:56.427Z | 337.258° NNW |
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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