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: 13 hours ago
TLE from 13 hours ago
0 LUNA-2
1 68470U 26067BG 26219.88641705 .00003301 00000-0 16581-3 0 9996
2 68470 97.4506 177.3336 0004948 241.7933 118.2801 15.17962348 19773Epoch: 2026-08-07T21:16Z
TLE epoch observation values (Epoch: 2026-08-07T21:16:26.433Z)
Latitude
-0.00006°
Longitude
-98.18221°
Altitude
516.703 km
Speed
7.604 km/s
True Right ascension
11h 49m 20s
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
00:04:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
512.378 km
Perigee altitude
505.562 km
Semi-major axis
6,887.107 km
Eccentricity
0.00049
Inclination
97.4506°
RAAN
177.3336°
Arg. of periapsis
241.7933°
True anomaly
118.33002°
Mean anomaly
118.2801°
Eccentric anomaly
118.30506°
Mean motion
3.79741 °/min
Orbital period
94.8 mins
BSTAR
0.00016581
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-08-08 10:29:09.696Z | 356.555° N | 2026-08-08 10:32:09.696Z | 296.64° NW | 34.235° | 2026-08-08 10:35:09.696Z | 218.497° SW |
| 5 mins | 2026-08-08 21:09:09.696Z | 153.712° SSE | 2026-08-08 21:11:09.696Z | 55.064° ENE | 43.026° | 2026-08-08 21:14:09.696Z | 353.816° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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