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LEMUR-2 WOBLER

NORAD 67368 Payload LEO 2026-004F ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
596 km
Apogee
606 km
Inclination
97.8°
Period
96.7 min
Mean Motion
14.89074281 rev/day
TLE Epoch
2026-09-16 10:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude601 km
Orbital Velocity27,220 km/h
Velocity7.56 km/s
Orbital Period97 minutes
Orbits / Day14.89
Eccentricity0.0007
Semi-Major Axis6,972 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇺🇸 Spire/Lux (United States)
Launch Date
2026-01-11
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
2026-004F
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
LEMUR-2 WOBLER is an active satellite operated by Spire/Lux (United States), launched on 2026-01-11 from Vandenberg Space Force Base, United States on the Twilight launch. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Low Earth Orbit (LEO) at altitudes between 596 km and 606 km with an inclination of 97.8°. It travels at approximately 27,220 km/h (7.56 km/s), completing one full orbit every 97 minutes — that’s roughly 14.89 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 ~10–25 years. Orbital Radar tracks LEMUR-2 WOBLER 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 WOBLER orbits at an average altitude of 601 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 WOBLER’s average altitude, there are currently 1,637 active payloads and 719 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050, STARLINK-3005, STARLINK-3090. This makes it one of the more crowded altitude bands, containing roughly 8.8% of all active satellites. With an inclination of 97.8°, LEMUR-2 WOBLER passes over latitudes between 97.8°N and 97.8°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 13,204 active satellites in total, of which 1,056 share a similar altitude band with LEMUR-2 WOBLER.
🔗 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 WOBLER is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 601 km altitude. Its 97.8° 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 97 minutes, travelling at 27,220 km/h.
LEMUR-2 WOBLER is operated by Spire/Lux (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 67368. You can track LEMUR-2 WOBLER in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
LEMUR-2 WOBLER was launched on 2026-01-11 from Vandenberg Space Force Base, United States, 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: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks LEMUR-2 WOBLER (NORAD ID 67368) 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 WOBLER travels at approximately 27,220 km/h (16,914 mph) — roughly 7.56 km/s. It completes 14.89 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.