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LEMUR 2 TOMATOKECHUP

NORAD 60471 Payload LEO 2024-149D ● Active
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🛰️ Orbital Parameters
Perigee
448 km
Apogee
452 km
Inclination
97.4°
Period
93.6 min
Mean Motion
15.38656198 rev/day
TLE Epoch
2026-11-01 23:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude450 km
Orbital Velocity27,520 km/h
Velocity7.64 km/s
Orbital Period94 minutes
Orbits / Day15.39
Eccentricity0.0003
Semi-Major Axis6,821 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇺🇸 SPIREG / Hubble Network (United States)
Launch Date
2024-08-16
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
2024-149D
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
LEMUR 2 TOMATOKECHUP is an active satellite operated by SPIREG / Hubble Network (United States), launched on 2024-08-16 from Vandenberg Space Force Base, United States on the Transporter-11 launch. It orbits in Low Earth Orbit (LEO) at altitudes between 448 km and 452 km with an inclination of 97.4°. It travels at approximately 27,520 km/h (7.64 km/s), completing one full orbit every 94 minutes — that’s roughly 15.39 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 ~1–3 years. Orbital Radar tracks LEMUR 2 TOMATOKECHUP 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 TOMATOKECHUP orbits at an average altitude of 450 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 TOMATOKECHUP’s average altitude, there are currently 10,560 active payloads and 157 tracked debris or rocket body fragments — notable neighbours include ISS (ZARYA), STARLINK-1017, STARLINK-1039. This makes it one of the more crowded altitude bands, containing roughly 55.7% of all active satellites. With an inclination of 97.4°, LEMUR 2 TOMATOKECHUP 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 13,340 active satellites in total, of which 10,164 share a similar altitude band with LEMUR 2 TOMATOKECHUP.
🔗 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 TOMATOKECHUP is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 450 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 94 minutes, travelling at 27,520 km/h.
LEMUR 2 TOMATOKECHUP is operated by SPIREG / Hubble Network (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 60471. You can track LEMUR 2 TOMATOKECHUP in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
LEMUR 2 TOMATOKECHUP was launched on 2024-08-16 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: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks LEMUR 2 TOMATOKECHUP (NORAD ID 60471) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). 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 TOMATOKECHUP travels at approximately 27,520 km/h (17,100 mph) — roughly 7.64 km/s. It completes 15.39 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.