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 05491U 71083 A 74190.12768409 .65898548 +6439501 +32670-3 0 04914
2 05491 033.1153 216.5442 0001373 317.5153 042.5428 16.47074794158794
| Epoch (UTC): | 09 July 1974 03:03:51 |
| Eccentricity: | 0.0001373 |
| inclination: | 33.1153° |
| perigee height: | 146 km |
| apogee height: | 148 km |
| right ascension of ascending node: | 216.5442° |
| argument of perigee: | 317.5153° |
| revolutions per day: | 16.47074794 |
| mean anomaly at epoch: | 42.5428° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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