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TOMS EP

NORAD 23940 Payload LEO 1996-037A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
675 km
Apogee
712 km
Inclination
98.5°
Period
98.6 min
Mean Motion
14.59920797 rev/day
TLE Epoch
2026-06-19 00:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude694 km
Orbital Velocity27,041 km/h
Velocity7.51 km/s
Orbital Period99 minutes
Orbits / Day14.60
Eccentricity0.0026
Semi-Major Axis7,065 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1996-07-02
Launch Site
Vandenberg SFB, California
Int'l Designator
1996-037A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
TOMS EP is an active satellite operated by United States, launched on 1996-07-02 from Vandenberg SFB, California. With over 30 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 675 km and 712 km with an inclination of 98.5°. It travels at approximately 27,041 km/h (7.51 km/s), completing one full orbit every 99 minutes — that’s roughly 14.60 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. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~10–25 years. Orbital Radar tracks TOMS EP in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
TOMS EP orbits at an average altitude of 694 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 TOMS EP’s average altitude, there are currently 281 active payloads and 1,369 tracked debris or rocket body fragments — notable neighbours include TERRA, AQUA, LANDSAT 9. With an inclination of 98.5°, TOMS EP passes over latitudes between 98.5°N and 98.5°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 60 share a similar altitude band with TOMS EP.
❓ Frequently Asked Questions
TOMS EP is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 694 km altitude. Its 98.5° 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 99 minutes, travelling at 27,041 km/h.
TOMS EP is operated by United States. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 23940. You can track TOMS EP in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
TOMS EP was launched on 1996-07-02 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: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks TOMS EP (NORAD ID 23940) 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.
TOMS EP travels at approximately 27,041 km/h (16,803 mph) — roughly 7.51 km/s. It completes 14.60 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.