SAR LUPE 2
NORAD 31797
Payload
LEO
2007-030A
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LEO · NORAD 31797
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
393 km
Apogee
402 km
Inclination
98.1°
Period
92.5 min
Mean Motion
15.56606318 rev/day
TLE Epoch
2026-08-03 22:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude398 km
Orbital Velocity27,626 km/h
Velocity7.67 km/s
Orbital Period93 minutes
Orbits / Day15.57
Eccentricity0.0007
Semi-Major Axis6,769 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital LifetimeMonths to ~1 year
🚀 Launch & Identity
Country / Operator
🇩🇪 Armed Forces (Germany)
Launch Date
2007-07-02
Launch Site
PKMTR
Int'l Designator
2007-030A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
SAR LUPE 2 is an active satellite operated by Armed Forces (Germany), launched on 2007-07-02 from PKMTR on the SAR-Lupe 2 launch. After 19 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 393 km and 402 km with an inclination of 98.1°. It travels at approximately 27,626 km/h (7.67 km/s), completing one full orbit every 93 minutes — that’s roughly 15.57 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 months to ~1 year. Orbital Radar tracks SAR LUPE 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
SAR LUPE 2 orbits at an average altitude of 398 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 SAR LUPE 2’s average altitude, there are currently 1,270 active payloads and 87 tracked debris or rocket body fragments — notable neighbours include STARLINK-1008, STARLINK-1012, STARLINK-1020. This makes it one of the more crowded altitude bands, containing roughly 7.1% of all active satellites. With an inclination of 98.1°, SAR LUPE 2 passes over latitudes between 98.1°N and 98.1°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. Germany operates approximately 87 active satellites in total, of which 9 share a similar altitude band with SAR LUPE 2.
❓ Frequently Asked Questions
SAR LUPE 2 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 398 km altitude. Its 98.1° 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 93 minutes, travelling at 27,626 km/h.
SAR LUPE 2 is operated by Armed Forces (Germany). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 31797. You can track SAR LUPE 2 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
SAR LUPE 2 was launched on 2007-07-02 from PKMTR. At its current altitude, the estimated remaining orbital lifetime is: months to ~1 year. View the full satellite launch log.
Yes — Orbital Radar tracks SAR LUPE 2 (NORAD ID 31797) 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.
SAR LUPE 2 travels at approximately 27,626 km/h (17,166 mph) — roughly 7.67 km/s. It completes 15.57 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.