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OPS 6553

NORAD 13172 Payload LEO 1982-041C ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
542 km
Apogee
553 km
Inclination
96.0°
Period
95.6 min
Mean Motion
15.06324938 rev/day
TLE Epoch
2026-06-19 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude548 km
Orbital Velocity27,325 km/h
Velocity7.59 km/s
Orbital Period96 minutes
Orbits / Day15.06
Eccentricity0.0008
Semi-Major Axis6,919 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1982-05-11
Launch Site
Vandenberg SFB, California
Int'l Designator
1982-041C
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
OPS 6553 is an active satellite operated by United States, launched on 1982-05-11 from Vandenberg SFB, California. With over 44 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 542 km and 553 km with an inclination of 96.0°. It travels at approximately 27,325 km/h (7.59 km/s), completing one full orbit every 96 minutes — that’s roughly 15.06 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 ~3–10 years. Orbital Radar tracks OPS 6553 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
OPS 6553 orbits at an average altitude of 548 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 OPS 6553’s average altitude, there are currently 3,476 active payloads and 355 tracked debris or rocket body fragments — notable neighbours include STARLINK-1184, STARLINK-1276, ONEWEB-0050. This makes it one of the more crowded altitude bands, containing roughly 20% of all active satellites. With an inclination of 96.0°, OPS 6553 passes over latitudes between 96.0°N and 96.0°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 2,822 share a similar altitude band with OPS 6553.
❓ Frequently Asked Questions
OPS 6553 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 548 km altitude. Its 96.0° 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 96 minutes, travelling at 27,325 km/h.
OPS 6553 is operated by United States. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 13172. You can track OPS 6553 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
OPS 6553 was launched on 1982-05-11 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: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks OPS 6553 (NORAD ID 13172) 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.
OPS 6553 travels at approximately 27,325 km/h (16,979 mph) — roughly 7.59 km/s. It completes 15.06 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.