NANOSAT 1B
Launch
Launched on Jul 29, 2009 from 109/95, Kazakhstan aboard a Dnepr 1.
Dnepr | DubaiSat 1 →Live · TLE epoch 2026-09-08 07:36 UTC
Orbit class
SSO — Sun-Synchronous (LEO at 96–102° inclination)
Operator
INTA
Country
Spain
Manufacturer
—
Launched
Jul 29, 2009
Mass
—
Apogee
625 km
Perigee
559 km
Inclination
98.13°
Period
1.61 h
Altitude history
Apogee and perigee for NANOSAT 1B across 14 days of archived orbital elements (15 element sets, one per day).
Trend
Stable
Change
-0.1 km
Rate
-0.01 km/day
Now
559 × 625 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.
Launched with
5 other catalogued objects still in orbit from launch 2009-041 (Dnepr | DubaiSat 1).
- DEIMOS-1 · 35681
- DUBAISAT-1 · 35682
- UK-DMC 2 · 35683
- APRIZESAT 4 · 35684
- APRIZESAT 3 · 35686
Sources & further reading
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