LEMUR-2-TEODOR
NORAD 66768
Payload
LEO
2025-276DG
● Active
CONNECTING…
LEO · NORAD 66768
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
501 km
Apogee
504 km
Inclination
97.4°
Period
94.7 min
Mean Motion
15.21068802 rev/day
TLE Epoch
2026-06-19 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude503 km
Orbital Velocity27,415 km/h
Velocity7.62 km/s
Orbital Period95 minutes
Orbits / Day15.21
Eccentricity0.0002
Semi-Major Axis6,874 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇺🇸 Spire Global (United States)
Launch Date
2025-11-28
Launch Site
Vandenberg SFB, California
Int'l Designator
2025-276DG
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
LEMUR-2-TEODOR is an active satellite operated by Spire Global (United States), 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 501 km and 504 km with an inclination of 97.4°. It travels at approximately 27,415 km/h (7.62 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 LEMUR-2-TEODOR in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
LEMUR-2-TEODOR orbits at an average altitude of 503 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 LEMUR-2-TEODOR’s average altitude, there are currently 9,586 active payloads and 247 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 55.1% of all active satellites. With an inclination of 97.4°, LEMUR-2-TEODOR 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. United States operates approximately 12,339 active satellites in total, of which 8,962 share a similar altitude band with LEMUR-2-TEODOR.
🔗 Spire Global Constellation
This satellite is part of Spire Global's constellation of 3U CubeSats collecting weather, maritime and aviation data through radio occultation, AIS and ADS-B payloads. Spire operates over 100 multi-purpose nanosatellites in LEO, providing atmospheric profiles used by weather agencies worldwide, global ship tracking and flight tracking services.
❓ Frequently Asked Questions
LEMUR-2-TEODOR is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 503 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 27,415 km/h.
LEMUR-2-TEODOR is operated by Spire Global (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 66768. You can track LEMUR-2-TEODOR in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
LEMUR-2-TEODOR 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 LEMUR-2-TEODOR (NORAD ID 66768) 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.
LEMUR-2-TEODOR travels at approximately 27,415 km/h (17,035 mph) — roughly 7.62 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.