LUNA-2, 68470
Orbit data source: Space-Track
LUNA-2, 68470 is a Turkish payload satellite 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
None
Manufacturer
Unknown
Mission
Operational spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 0.2 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 LUNA-2
1 68470U 26067BG 26171.42753731 .00004773 00000-0 24157-3 0 9998
2 68470 97.4479 129.6452 0008724 65.1489 295.0650 15.17459084 12420Epoch: 2026-06-20T10:15Z
TLE epoch observation values (Epoch: 2026-06-20T10:15:39.223Z)
Latitude
-0.00011°
Longitude
67.08947°
Altitude
514.065 km
Speed
7.608 km/s
True Right ascension
08h 38m 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
09:13:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
516.504 km
Perigee altitude
504.484 km
Semi-major axis
6,888.631 km
Eccentricity
0.00087
Inclination
97.4479°
RAAN
129.6452°
Arg. of periapsis
65.1489°
True anomaly
294.9744°
Mean anomaly
295.065°
Eccentric anomaly
295.01971°
Mean motion
3.79615 °/min
Orbital period
94.83 mins
BSTAR
0.00024157
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-22 10:17:29.349Z | 4.682° NNE | 2026-06-22 10:20:29.349Z | 322.974° NNW | 39.898° | 2026-06-22 10:24:29.349Z | 203.714° SW |
| 5 mins | 2026-06-22 20:57:29.349Z | 141.825° SSE | 2026-06-22 20:59:29.349Z | 93.567° ESE | 35.917° | 2026-06-22 21:02:29.349Z | 4.358° NNE |
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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