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Home Library Satellite Directory DMSP 5D-2 F10 (USA 68)

DMSP 5D-2 F10 (USA 68)

NORAD 20978 Payload LEO 1990-105A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
708 km
Apogee
808 km
Inclination
98.6°
Period
100.0 min
Mean Motion
14.40164684 rev/day
TLE Epoch
2026-06-19 03:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude758 km
Orbital Velocity26,919 km/h
Velocity7.48 km/s
Orbital Period100 minutes
Orbits / Day14.40
Eccentricity0.0070
Semi-Major Axis7,129 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1990-12-01
Launch Site
Vandenberg SFB, California
Int'l Designator
1990-105A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
DMSP 5D-2 F10 (USA 68) is an active satellite operated by United States, launched on 1990-12-01 from Vandenberg SFB, California. With over 36 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 708 km and 808 km with an inclination of 98.6°. It travels at approximately 26,919 km/h (7.48 km/s), completing one full orbit every 100 minutes — that’s roughly 14.40 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 ~25–100 years. Orbital Radar tracks DMSP 5D-2 F10 (USA 68) in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
DMSP 5D-2 F10 (USA 68) orbits at an average altitude of 758 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 DMSP 5D-2 F10 (USA 68)’s average altitude, there are currently 357 active payloads and 2,018 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0179. With an inclination of 98.6°, DMSP 5D-2 F10 (USA 68) passes over latitudes between 98.6°N and 98.6°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 147 share a similar altitude band with DMSP 5D-2 F10 (USA 68).
❓ Frequently Asked Questions
DMSP 5D-2 F10 (USA 68) is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 758 km altitude. Its 98.6° 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 100 minutes, travelling at 26,919 km/h.
DMSP 5D-2 F10 (USA 68) is operated by United States. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 20978. You can track DMSP 5D-2 F10 (USA 68) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
DMSP 5D-2 F10 (USA 68) was launched on 1990-12-01 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: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks DMSP 5D-2 F10 (USA 68) (NORAD ID 20978) 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.
DMSP 5D-2 F10 (USA 68) travels at approximately 26,919 km/h (16,727 mph) — roughly 7.48 km/s. It completes 14.40 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.