SL-16 R/B
Launch
Launched on Nov 4, 1994 from 45/1, Kazakhstan aboard a Zenit-2.
Zenit-2 | Resurs-O1 →Live · TLE epoch 2026-09-09 15:03 UTC
Orbit class
SSO — Sun-Synchronous (LEO at 96–102° inclination)
Operator
Russian / Soviet Government
Country
Russia
Manufacturer
—
Launched
Nov 4, 1994
Mass
—
Apogee
639 km
Perigee
630 km
Inclination
97.70°
Period
1.62 h
Altitude history
Apogee and perigee for SL-16 R/B across 103 days of archived orbital elements (105 element sets, one per day).
Trend
Stable
Change
-0.2 km
Rate
-0.00 km/day
Now
630 × 639 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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