SL-16 R/B
Launch
Launched on May 15, 1988 from 45/1, Kazakhstan aboard a Zenit-2.
Zenit-2 | Tselina-2 5 →Live · TLE epoch 2026-09-08 16:31 UTC
Orbit class
LEO — Low Earth Orbit (circular, < 2,000 km)
Operator
Russian / Soviet Government
Country
Russia
Manufacturer
—
Launched
May 15, 1988
Mass
—
Apogee
846 km
Perigee
817 km
Inclination
71.02°
Period
1.69 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
-0.0 km
Rate
-0.00 km/day
Now
817 × 846 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.
Related satellites
Sources & further reading
Embed this satellite on your site
Free for editorial use. Attribution back to LowEarth is required.
<iframe src="https://lowearth.app/embed/19120" width="640" height="400" frameborder="0" allow="fullscreen"></iframe>