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 22065U 92049 B 93175.71348247 .00004426 +00000-0 +14314-3 01219
2 22065 028.4600 291.5904 0005617 196.6864 163.3548 15.29184886050003
| Epoch (UTC): | 24 June 1993 17:07:24 |
| Eccentricity: | 0.0005617 |
| inclination: | 28.4600° |
| perigee height: | 474 km |
| apogee height: | 482 km |
| right ascension of ascending node: | 291.5904° |
| argument of perigee: | 196.6864° |
| revolutions per day: | 15.29184886 |
| mean anomaly at epoch: | 163.3548° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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