CHAMRAN-1
Launch
Launched on Sep 14, 2024 from Launch Platform, Iran aboard a Qaem 100.
Qaem 100 | Chamran-1 →Live · TLE epoch 2026-10-23 19:44 UTC
Orbit class
LEO — Low Earth Orbit (circular, < 2,000 km)
Operator
—
Country
Iran
Manufacturer
—
Launched
Sep 14, 2024
Mass
—
Apogee
580 km
Perigee
492 km
Inclination
64.08°
Period
1.59 h
Altitude history
Apogee and perigee for CHAMRAN-1 across 59 days of archived orbital elements (60 element sets, one per day).
Trend
Decaying
Change
-1.2 km
Rate
-0.02 km/day
Now
492 × 580 km
Apogee Perigee
Derived from our own archive of CelesTrak orbital elements, sampled every 3 hours. Short windows show drag and station-keeping; they are not a reentry prediction.
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