SL-5 R/B
- SL-5 R/B SL-5 R/B
Object Name SL-5 R/B
Object Full Name -
Norad ID 783
Cospar ID 1964-019B
Object Type Rocket body or debris
Object Status Decayed
Object Class -
End of Life -

Polyot 2 was the second of two spacecraft fitted with special controls to allow for maneuverability in space. The spacecraft was able to change inclination as well as apogee and perigee. It also carried scientific instruments, a telemetry system, and radio transmitters.

Launch Date 1964-04-12
Decay Date 1964-05-08
Launch Vehicle -
Launch Site Baikonur Cosmodrome, Kazakhstan
Launch Provider -
Launch Provider Country -
Launch Mass -
Dry Mass -
User -
Mission -
Mission Detail -
Country of Registry -
Programme -
Operator -
Country of Operator USSR/Russia
Contractor -
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Payload Contractor -
Payload Contractor Country -
Orbit Status Earth Orbit
Orbit -
Orbit Type -
Period: 90.5 min
Inclination: 59.9°
Apogee: 372.0 km
Perigee: 226.0 km
Longitude of Geo -
ECT -
Payload -
Platform -
Propulsion -
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Power -
Budget -
Call Sign -
Beacon -
RCS -
References -
Date
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Pass Time
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Time
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									Angular Momentum:
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									Eccentricity:
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									Inclination:
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									RAAN:
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									Argument of Perigee:
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									True Anomaly:
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									Period:
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									Semi-Major Axis:
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									Perigee:
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									Apogee:
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									Mean Motion:
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									Mean Anomaly:
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									Latitude:
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									Longitude:
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									Altitude:
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									Speed:
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									Azimuth:
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									Elevation:
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									Range:
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