LUNA-2, 68470
Orbit data source: Space-Track
LUNA-2, 68470 is a payload satellite owned by Aselsan (TR) 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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68470 intel report (Beta)
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Identifier
Orbit
Country
TR / TURKRelated business
Manufacturer
Aselsan
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 6U?, Unknown motor
Mass
~12 kg wet, ~12 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 LUNA-2
1 68470U 26067BG 26217.38145099 .00004345 00000-0 21733-3 0 9998
2 68470 97.4507 174.8667 0004828 253.6314 106.4389 15.17944656 19395Epoch: 2026-08-05T09:09Z
TLE epoch observation values (Epoch: 2026-08-05T09:09:17.365Z)
Latitude
-0.00005°
Longitude
83.60769°
Altitude
516.083 km
Speed
7.605 km/s
True Right ascension
11h 39m 28s
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
16:18:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
512.349 km
Perigee altitude
505.699 km
Semi-major axis
6,887.161 km
Eccentricity
0.00048
Inclination
97.4507°
RAAN
174.8667°
Arg. of periapsis
253.6314°
True anomaly
106.49195°
Mean anomaly
106.4389°
Eccentric anomaly
106.46543°
Mean motion
3.79737 °/min
Orbital period
94.8 mins
BSTAR
0.00021733
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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.LUNA-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 | 2026-08-06 09:27:38.050Z | 41.587° NE | 2026-08-06 09:30:38.050Z | 105.66° ESE | 24.247° | 2026-08-06 09:32:38.050Z | 146.995° SSE |
| 4 mins | 2026-08-06 11:02:38.050Z | 320.603° NNW | 2026-08-06 11:03:38.050Z | 301.639° NW | 17.157° | 2026-08-06 11:06:38.050Z | 247.788° W |
| 5 mins | 2026-08-06 21:40:38.050Z | 197.776° SSW | 2026-08-06 21:42:38.050Z | 246.165° WSW | 33.349° | 2026-08-06 21:45:38.050Z | 328.001° 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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