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 08062U 75072A 78135.61213027 +.00000415 +00000-0 +00000-0 0 00028
2 08062 096.5438 040.4972 7081866 304.4967 118.4376 00.65379857001357
| Epoch (UTC): | 15 May 1978 14:41:28 |
| Eccentricity: | 0.7081866 |
| inclination: | 96.5438° |
| perigee height: | 9985 km |
| apogee height: | 89409 km |
| right ascension of ascending node: | 40.4972° |
| argument of perigee: | 304.4967° |
| revolutions per day: | 0.65379857 |
| mean anomaly at epoch: | 118.4376° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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