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SAPPHIRE

NORAD 26932 Payload LEO 2001-043D ● Active
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🛰️ Orbital Parameters
Perigee
784 km
Apogee
791 km
Inclination
67.1°
Period
100.6 min
Mean Motion
14.31323948 rev/day
TLE Epoch
2026-11-02 03:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude788 km
Orbital Velocity26,863 km/h
Velocity7.46 km/s
Orbital Period101 minutes
Orbits / Day14.31
Eccentricity0.0005
Semi-Major Axis7,159 km
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇺🇸 USNA / Stanford (United States)
Launch Date
2001-09-30
Launch Site
Pacific Spaceport Complex Alaska, United States
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 USNA / Stanford (United States), launched on 2001-09-30 from Pacific Spaceport Complex Alaska, United States on the Starshine 3 launch. With over 25 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 784 km and 791 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 435 active payloads and 2,479 tracked debris or rocket body fragments — notable neighbours include NOAA 20, 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 13,340 active satellites in total, of which 187 share a similar altitude band with SAPPHIRE.
❓ Frequently Asked Questions
SAPPHIRE orbits in Low Earth Orbit (LEO) at altitudes between 784 km (perigee) and 791 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 USNA / Stanford (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 Pacific Spaceport Complex Alaska, United States. 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) orbital data in its live tracking catalogue (see our data sources). 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.