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LEMUR 2 OBA-NI-JESU

NORAD 58902 Payload LEO 2024-022D ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
168 km
Apogee
180 km
Inclination
97.4°
Period
88.0 min
Mean Motion
16.36778297 rev/day
TLE Epoch
2026-06-13 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude174 km
Orbital Velocity28,094 km/h
Velocity7.80 km/s
Orbital Period88 minutes
Orbits / Day16.37
Eccentricity0.0009
Semi-Major Axis6,545 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital LifetimeDays to weeks — very low orbit, rapid decay
🚀 Launch & Identity
Country / Operator
🇺🇸 Spire Global (United States)
Launch Date
2024-01-31
Launch Site
RLLC
Int'l Designator
2024-022D
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
LEMUR 2 OBA-NI-JESU is an active satellite operated by Spire Global (United States), launched on 2024-01-31 from RLLC. It orbits in Low Earth Orbit (LEO) at altitudes between 168 km and 180 km with an inclination of 97.4°. It travels at approximately 28,094 km/h (7.80 km/s), completing one full orbit every 88 minutes — that’s roughly 16.37 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 days to weeks — very low orbit, rapid decay. Orbital Radar tracks LEMUR 2 OBA-NI-JESU 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 OBA-NI-JESU orbits at an average altitude of 174 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 OBA-NI-JESU’s average altitude, there are currently 6 active payloads and 0 tracked debris or rocket body fragments — notable neighbours include STARLINK-3633, STARLINK-5160. This is a relatively sparse altitude band, containing less than 1% of all active satellites. With an inclination of 97.4°, LEMUR 2 OBA-NI-JESU 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 6 share a similar altitude band with LEMUR 2 OBA-NI-JESU.
🔗 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 OBA-NI-JESU is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 174 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 88 minutes, travelling at 28,094 km/h.
LEMUR 2 OBA-NI-JESU is operated by Spire Global (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 58902. You can track LEMUR 2 OBA-NI-JESU in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
LEMUR 2 OBA-NI-JESU was launched on 2024-01-31 from RLLC. At its current altitude, the estimated remaining orbital lifetime is: days to weeks — very low orbit, rapid decay. View the full satellite launch log.
Yes — Orbital Radar tracks LEMUR 2 OBA-NI-JESU (NORAD ID 58902) 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 OBA-NI-JESU travels at approximately 28,094 km/h (17,457 mph) — roughly 7.80 km/s. It completes 16.37 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 33 sunrises and sunsets every 24 hours.