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KHAYYAM

NORAD 53370 Payload LEO 2022-096A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
487 km
Apogee
490 km
Inclination
97.3°
Period
94.4 min
Mean Motion
15.25780031 rev/day
TLE Epoch
2026-06-19 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude489 km
Orbital Velocity27,443 km/h
Velocity7.62 km/s
Orbital Period94 minutes
Orbits / Day15.26
Eccentricity0.0002
Semi-Major Axis6,860 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
Revolutionary Guard Corps (Iran)
Launch Date
2022-08-09
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2022-096A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
KHAYYAM is an active satellite operated by Revolutionary Guard Corps (Iran), launched on 2022-08-09 from Baikonur, Kazakhstan. It orbits in Low Earth Orbit (LEO) at altitudes between 487 km and 490 km with an inclination of 97.3°. It travels at approximately 27,443 km/h (7.62 km/s), completing one full orbit every 94 minutes — that’s roughly 15.26 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 ~1–3 years. Orbital Radar tracks KHAYYAM in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
KHAYYAM orbits at an average altitude of 489 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 KHAYYAM’s average altitude, there are currently 8,099 active payloads and 228 tracked debris or rocket body fragments — notable neighbours include STARLINK-1017, STARLINK-1039, STARLINK-1047. This makes it one of the more crowded altitude bands, containing roughly 46.5% of all active satellites. With an inclination of 97.3°, KHAYYAM passes over latitudes between 97.3°N and 97.3°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. Iran operates approximately 5 active satellites in total, of which 2 share a similar altitude band with KHAYYAM.
❓ Frequently Asked Questions
KHAYYAM is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 489 km altitude. Its 97.3° 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 94 minutes, travelling at 27,443 km/h.
KHAYYAM is operated by Revolutionary Guard Corps (Iran). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 53370. You can track KHAYYAM in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
KHAYYAM was launched on 2022-08-09 from Baikonur, Kazakhstan, the world’s first and largest operational space launch facility, located in Kazakhstan. At its current altitude, the estimated remaining orbital lifetime is: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks KHAYYAM (NORAD ID 53370) 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.
KHAYYAM travels at approximately 27,443 km/h (17,052 mph) — roughly 7.62 km/s. It completes 15.26 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.