View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 05128U 71030 A 80028.58692431 .18043179 +50138-4 +23760-3 0 9998
2 05128 046.3144 182.7352 0002710 254.7670 105.2979 16.43432022485264
| Epoch (UTC): | 28 January 1980 14:05:10 |
| Eccentricity: | 0.0002710 |
| inclination: | 46.3144° |
| perigee height: | 155 km |
| apogee height: | 158 km |
| right ascension of ascending node: | 182.7352° |
| argument of perigee: | 254.7670° |
| revolutions per day: | 16.43432022 |
| mean anomaly at epoch: | 105.2979° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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