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MICE-1

NORAD 66684 Payload LEO 2025-276U ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
505 km
Apogee
512 km
Inclination
97.4°
Period
94.8 min
Mean Motion
15.19202197 rev/day
TLE Epoch
2026-06-19 03:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude509 km
Orbital Velocity27,403 km/h
Velocity7.61 km/s
Orbital Period95 minutes
Orbits / Day15.19
Eccentricity0.0005
Semi-Major Axis6,880 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
GREC
Launch Date
2025-11-28
Launch Site
Vandenberg SFB, California
Int'l Designator
2025-276U
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
MICE-1 is an active satellite operated by GREC, launched on 2025-11-28 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 505 km and 512 km with an inclination of 97.4°. It travels at approximately 27,403 km/h (7.61 km/s), completing one full orbit every 95 minutes — that’s roughly 15.19 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 MICE-1 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
MICE-1 orbits at an average altitude of 509 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 MICE-1’s average altitude, there are currently 9,540 active payloads and 263 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 54.8% of all active satellites. With an inclination of 97.4°, MICE-1 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. GREC operates approximately 10 active satellites in total, of which 6 share a similar altitude band with MICE-1.
❓ Frequently Asked Questions
MICE-1 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 509 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 27,403 km/h.
MICE-1 is operated by GREC. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 66684. You can track MICE-1 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
MICE-1 was launched on 2025-11-28 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 MICE-1 (NORAD ID 66684) 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.
MICE-1 travels at approximately 27,403 km/h (17,027 mph) — roughly 7.61 km/s. It completes 15.19 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.