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 05007U 71018 A 79167.98634384 .07111837 +00000-0 +00000-0 0 9992
2 05007 069.7897 133.7887 0016976 337.3082 029.8532 16.45643152433053
| Epoch (UTC): | 16 June 1979 23:40:20 |
| Eccentricity: | 0.0016976 |
| inclination: | 69.7897° |
| perigee height: | 140 km |
| apogee height: | 162 km |
| right ascension of ascending node: | 133.7887° |
| argument of perigee: | 337.3082° |
| revolutions per day: | 16.45643152 |
| mean anomaly at epoch: | 29.8532° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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