LEMUR 2 THEFALCONER
NORAD 63264
Payload
LEO
2025-052BG
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LEO · NORAD 63264
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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
573 km
Apogee
577 km
Inclination
97.7°
Period
96.2 min
Mean Motion
14.97398279 rev/day
TLE Epoch
2026-06-19 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude575 km
Orbital Velocity27,271 km/h
Velocity7.58 km/s
Orbital Period96 minutes
Orbits / Day14.97
Eccentricity0.0003
Semi-Major Axis6,946 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇺🇸 Spire Global (United States)
Launch Date
2025-03-15
Launch Site
Vandenberg SFB, California
Int'l Designator
2025-052BG
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
LEMUR 2 THEFALCONER is an active satellite operated by Spire Global (United States), launched on 2025-03-15 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 573 km and 577 km with an inclination of 97.7°. It travels at approximately 27,271 km/h (7.58 km/s), completing one full orbit every 96 minutes — that’s roughly 14.97 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 THEFALCONER 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 THEFALCONER orbits at an average altitude of 575 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 THEFALCONER’s average altitude, there are currently 3,165 active payloads and 502 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050, STARLINK-1522, STARLINK-2112. This makes it one of the more crowded altitude bands, containing roughly 18.2% of all active satellites. With an inclination of 97.7°, LEMUR 2 THEFALCONER passes over latitudes between 97.7°N and 97.7°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 2,613 share a similar altitude band with LEMUR 2 THEFALCONER.
🔗 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 THEFALCONER is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 575 km altitude. Its 97.7° 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 96 minutes, travelling at 27,271 km/h.
LEMUR 2 THEFALCONER is operated by Spire Global (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 63264. You can track LEMUR 2 THEFALCONER in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
LEMUR 2 THEFALCONER was launched on 2025-03-15 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 THEFALCONER (NORAD ID 63264) 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 THEFALCONER travels at approximately 27,271 km/h (16,946 mph) — roughly 7.58 km/s. It completes 14.97 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.