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EOS-5

NORAD 100607 Payload MEO 2026-202A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
154 km
Apogee
30963 km
Inclination
19.3°
Period
538.9 min
Mean Motion
2.67302545 rev/day
TLE Epoch
2026-09-04 20:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude15,559 km
Orbital Velocity15,348 km/h
Velocity4.26 km/s
Orbital Period8 hours 59 minutes
Orbits / Day2.67
Eccentricity0.7025
Semi-Major Axis21,930 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇮🇳 India
Launch Date
2026-09-03
Launch Site
SRI
Int'l Designator
2026-202A
Object Type
Payload
RCS Size
Unknown
📖 About This Object
EOS-5 is an active satellite operated by India, launched on 2026-09-03 from SRI on the GISAT-1A launch. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Medium Earth Orbit (MEO) at altitudes between 154 km and 30,963 km with an inclination of 19.3°. It travels at approximately 15,348 km/h (4.26 km/s), completing one full orbit every 8 hours 59 minutes — that’s roughly 2.67 orbits per day. Its orbital eccentricity of 0.7025 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Orbital Radar tracks EOS-5 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
EOS-5 orbits at an average altitude of 15,559 km in Medium Earth Orbit, the region between LEO and GEO (2,000–35,786 km). MEO’s higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer spacecraft are needed for global coverage — but signal latency is higher and radiation from the Van Allen belts is a significant design constraint. Within ±50 km of EOS-5’s average altitude, there are currently 2 active payloads and 10 tracked debris or rocket body fragments. This is a relatively sparse altitude band, containing less than 1% of all active satellites. With an inclination of 19.3°, EOS-5 passes over latitudes between 19.3°N and 19.3°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. India operates approximately 109 active satellites in total.
❓ Frequently Asked Questions
EOS-5 orbits in Medium Earth Orbit (MEO) at altitudes between 154 km (perigee) and 30,963 km (apogee), with an average altitude of approximately 15,559 km. It completes one orbit every 8 hours 59 minutes, travelling at approximately 15,348 km/h (9,537 mph).
EOS-5 is operated by India. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 100607. You can track EOS-5 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
EOS-5 was launched on 2026-09-03 from SRI. At its current altitude, the estimated remaining orbital lifetime is: effectively permanent — above atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks EOS-5 (NORAD ID 100607) 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.
EOS-5 travels at approximately 15,348 km/h (9,537 mph) — roughly 4.26 km/s. It completes 2.67 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 5 sunrises and sunsets every 24 hours.