LUNA-2
NORAD 68470
Payload
LEO
2026-067BG
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LEO · NORAD 68470
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Altitude (km)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
507 km
Apogee
520 km
Inclination
97.5°
Period
94.9 min
Mean Motion
15.17443505 rev/day
TLE Epoch
2026-06-18 18:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude514 km
Orbital Velocity27,393 km/h
Velocity7.61 km/s
Orbital Period95 minutes
Orbits / Day15.17
Eccentricity0.0009
Semi-Major Axis6,885 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
Turkey
Launch Date
2026-03-30
Launch Site
Vandenberg SFB, California
Int'l Designator
2026-067BG
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
LUNA-2 is an active satellite operated by Turkey, launched on 2026-03-30 from Vandenberg SFB, California. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Low Earth Orbit (LEO) at altitudes between 507 km and 520 km with an inclination of 97.5°. It travels at approximately 27,393 km/h (7.61 km/s), completing one full orbit every 95 minutes — that’s roughly 15.17 orbits per day. Its near-polar, sun-synchronous orbit means it passes over any given point on Earth at approximately the same local solar time, ideal for consistent Earth observation lighting conditions. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~3–10 years. Orbital Radar tracks LUNA-2 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
LUNA-2 orbits at an average altitude of 514 km in a sun-synchronous orbit (SSO), a specialised subset of LEO where the orbital plane precesses to maintain a constant angle relative to the Sun. This provides consistent lighting conditions on every pass — essential for Earth observation, weather monitoring and environmental science. Within ±50 km of LUNA-2’s average altitude, there are currently 8,327 active payloads and 268 tracked debris or rocket body fragments — notable neighbours include STARLINK-1017, STARLINK-1039, STARLINK-1184. This makes it one of the more crowded altitude bands, containing roughly 47.8% of all active satellites. With an inclination of 97.5°, LUNA-2 passes over latitudes between 97.5°N and 97.5°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. Turkey operates approximately 41 active satellites in total, of which 19 share a similar altitude band with LUNA-2.
❓ Frequently Asked Questions
LUNA-2 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 514 km altitude. Its 97.5° inclination causes the orbital plane to precess at exactly the rate of the Earth’s revolution around the Sun, so the satellite crosses each latitude at a consistent local solar time. It completes one orbit every 95 minutes, travelling at 27,393 km/h.
LUNA-2 is operated by Turkey. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 68470. You can track LUNA-2 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
LUNA-2 was launched on 2026-03-30 from Vandenberg SFB, California, primarily used for polar and sun-synchronous orbit launches due to its southward ocean trajectory from California. At its current altitude, the estimated remaining orbital lifetime is: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks LUNA-2 (NORAD ID 68470) using the latest TLE (two-line element set) data from Space-Track and CelesTrak. Open the live tracker to see its current position, altitude, speed and orbital path updated in real time. You can also browse the satellite directory to find other tracked objects.
LUNA-2 travels at approximately 27,393 km/h (17,021 mph) — roughly 7.61 km/s. It completes 15.17 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.