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EUCROPIS

NORAD 43807 Payload LEO 2018-099BB ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
501 km
Apogee
507 km
Inclination
97.4°
Period
94.7 min
Mean Motion
15.20611100 rev/day
TLE Epoch
2026-06-19 16:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude504 km
Orbital Velocity27,412 km/h
Velocity7.61 km/s
Orbital Period95 minutes
Orbits / Day15.21
Eccentricity0.0004
Semi-Major Axis6,875 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇩🇪 German Aerospace Center (DLR) (Germany)
Launch Date
2018-12-03
Launch Site
Vandenberg SFB, California
Int'l Designator
2018-099BB
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
EUCROPIS is an active satellite operated by German Aerospace Center (DLR) (Germany), launched on 2018-12-03 from Vandenberg SFB, California. It orbits in Low Earth Orbit (LEO) at altitudes between 501 km and 507 km with an inclination of 97.4°. It travels at approximately 27,412 km/h (7.61 km/s), completing one full orbit every 95 minutes — that’s roughly 15.21 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 EUCROPIS in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
EUCROPIS orbits at an average altitude of 504 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 EUCROPIS’s average altitude, there are currently 9,583 active payloads and 251 tracked debris or rocket body fragments — notable neighbours include STARLINK-1017, STARLINK-1039, STARLINK-1047. This makes it one of the more crowded altitude bands, containing roughly 55% of all active satellites. With an inclination of 97.4°, EUCROPIS passes over latitudes between 97.4°N and 97.4°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 80 active satellites in total, of which 26 share a similar altitude band with EUCROPIS.
❓ Frequently Asked Questions
EUCROPIS is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 504 km altitude. Its 97.4° 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 27,412 km/h.
EUCROPIS is operated by German Aerospace Center (DLR) (Germany). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 43807. You can track EUCROPIS in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
EUCROPIS was launched on 2018-12-03 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 EUCROPIS (NORAD ID 43807) 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.
EUCROPIS travels at approximately 27,412 km/h (17,033 mph) — roughly 7.61 km/s. It completes 15.21 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.