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 06285U 72092 A 74102.56081435 .01995071 +19882-1 +10878-2 0 9994
2 06285 091.0541 197.0816 0059827 070.1195 290.6485 16.21316685076432
| Epoch (UTC): | 12 April 1974 13:27:34 |
| Eccentricity: | 0.0059827 |
| inclination: | 91.0541° |
| perigee height: | 176 km |
| apogee height: | 255 km |
| right ascension of ascending node: | 197.0816° |
| argument of perigee: | 70.1195° |
| revolutions per day: | 16.21316685 |
| mean anomaly at epoch: | 290.6485° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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