SAPPHIRE
NORAD 26932
Payload
LEO
2001-043D
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LEO · NORAD 26932
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
783 km
Apogee
792 km
Inclination
67.1°
Period
100.6 min
Mean Motion
14.31295198 rev/day
TLE Epoch
2026-06-19 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude788 km
Orbital Velocity26,863 km/h
Velocity7.46 km/s
Orbital Period101 minutes
Orbits / Day14.31
Eccentricity0.0006
Semi-Major Axis7,159 km
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
2001-09-30
Launch Site
Kodiak, Alaska
Int'l Designator
2001-043D
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
SAPPHIRE is an active satellite operated by United States, launched on 2001-09-30 from Kodiak, Alaska. With over 25 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 783 km and 792 km with an inclination of 67.1°. It travels at approximately 26,863 km/h (7.46 km/s), completing one full orbit every 101 minutes — that’s roughly 14.31 orbits per day. 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 ~25–100 years. Orbital Radar tracks SAPPHIRE in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
SAPPHIRE orbits at an average altitude of 788 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 SAPPHIRE’s average altitude, there are currently 401 active payloads and 2,229 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0179, ONEWEB-0455. With an inclination of 67.1°, SAPPHIRE passes over latitudes between 67.1°N and 67.1°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. United States operates approximately 12,339 active satellites in total, of which 155 share a similar altitude band with SAPPHIRE.
❓ Frequently Asked Questions
SAPPHIRE orbits in Low Earth Orbit (LEO) at altitudes between 783 km (perigee) and 792 km (apogee), with an average altitude of approximately 788 km. It completes one orbit every 101 minutes, travelling at approximately 26,863 km/h (16,692 mph).
SAPPHIRE is operated by United States. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 26932. You can track SAPPHIRE in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
SAPPHIRE was launched on 2001-09-30 from Kodiak, Alaska. At its current altitude, the estimated remaining orbital lifetime is: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks SAPPHIRE (NORAD ID 26932) 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.
SAPPHIRE travels at approximately 26,863 km/h (16,692 mph) — roughly 7.46 km/s. It completes 14.31 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.