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UPM/LBSAT

NORAD 23607 Payload LEO 1995-033C ● Active
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🛰️ Orbital Parameters
Perigee
609 km
Apogee
618 km
Inclination
98.3°
Period
97.0 min
Mean Motion
14.84995269 rev/day
TLE Epoch
2026-10-31 18:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude614 km
Orbital Velocity27,196 km/h
Velocity7.55 km/s
Orbital Period97 minutes
Orbits / Day14.85
Eccentricity0.0006
Semi-Major Axis6,985 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇪🇸 IDR/UPM (Spain)
Launch Date
1995-07-07
Launch Site
Guiana Space Centre, French Guiana
Int'l Designator
1995-033C
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
UPM/LBSAT is an active satellite operated by IDR/UPM (Spain), launched on 1995-07-07 from Guiana Space Centre, French Guiana on the Helios 1A launch. With over 31 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 609 km and 618 km with an inclination of 98.3°. It travels at approximately 27,196 km/h (7.55 km/s), completing one full orbit every 97 minutes — that’s roughly 14.85 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 UPM/LBSAT in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
UPM/LBSAT orbits at an average altitude of 614 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 UPM/LBSAT’s average altitude, there are currently 1,288 active payloads and 786 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050, STARLINK-3055, STARLINK-3109. This makes it one of the more crowded altitude bands, containing roughly 6.8% of all active satellites. With an inclination of 98.3°, UPM/LBSAT passes over latitudes between 98.3°N and 98.3°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. Spain operates approximately 63 active satellites in total, of which 15 share a similar altitude band with UPM/LBSAT.
❓ Frequently Asked Questions
UPM/LBSAT is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 614 km altitude. Its 98.3° 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 27,196 km/h.
UPM/LBSAT is operated by IDR/UPM (Spain). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 23607. You can track UPM/LBSAT in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
UPM/LBSAT was launched on 1995-07-07 from Guiana Space Centre, French Guiana. At its current altitude, the estimated remaining orbital lifetime is: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks UPM/LBSAT (NORAD ID 23607) 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.
UPM/LBSAT travels at approximately 27,196 km/h (16,899 mph) — roughly 7.55 km/s. It completes 14.85 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.