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SEDSAT 1

NORAD 25509 Payload LEO 1998-061B ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
540 km
Apogee
1021 km
Inclination
31.4°
Period
100.5 min
Mean Motion
14.33389634 rev/day
TLE Epoch
2026-06-19 12:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude781 km
Orbital Velocity26,877 km/h
Velocity7.47 km/s
Orbital Period100 minutes
Orbits / Day14.33
Eccentricity0.0336
Semi-Major Axis7,152 km
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1998-10-24
Launch Site
Cape Canaveral, Florida
Int'l Designator
1998-061B
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
SEDSAT 1 is an active satellite operated by United States, launched on 1998-10-24 from Cape Canaveral, Florida. With over 28 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 540 km and 1,021 km with an inclination of 31.4°. It travels at approximately 26,877 km/h (7.47 km/s), completing one full orbit every 100 minutes — that’s roughly 14.33 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~25–100 years. Orbital Radar tracks SEDSAT 1 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
SEDSAT 1 orbits at an average altitude of 781 km in the mid-LEO band, where atmospheric drag is minimal but radiation exposure remains manageable. Objects at this altitude persist for decades to centuries, making debris mitigation critical. This regime is popular for remote sensing constellations and scientific instruments that need stable, long-duration orbits. Within ±50 km of SEDSAT 1’s average altitude, there are currently 417 active payloads and 2,197 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0179, ONEWEB-0455. With an inclination of 31.4°, SEDSAT 1 passes over latitudes between 31.4°N and 31.4°S, covering the tropical and temperate zones where most of the world’s population resides. Low-to-mid inclination orbits are efficient to reach from equatorial and mid-latitude launch sites. United States operates approximately 12,360 active satellites in total, of which 154 share a similar altitude band with SEDSAT 1.
❓ Frequently Asked Questions
SEDSAT 1 orbits in Low Earth Orbit (LEO) at altitudes between 540 km (perigee) and 1,021 km (apogee), with an average altitude of approximately 781 km. It completes one orbit every 100 minutes, travelling at approximately 26,877 km/h (16,700 mph).
SEDSAT 1 is operated by United States. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 25509. You can track SEDSAT 1 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
SEDSAT 1 was launched on 1998-10-24 from Cape Canaveral, Florida, one of the busiest launch facilities in the world, operated by NASA and the U.S. Space Force on Florida’s Atlantic coast. At its current altitude, the estimated remaining orbital lifetime is: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks SEDSAT 1 (NORAD ID 25509) 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.
SEDSAT 1 travels at approximately 26,877 km/h (16,700 mph) — roughly 7.47 km/s. It completes 14.33 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.