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 22640U 93027 A 93126.25000000 .00045476 +00000-0 +12392-3 0 9999
2 22640 028.4572 196.9260 0015496 336.8767 318.3931 15.92441940001538
| Epoch (UTC): | 06 May 1993 06:00:00 |
| Eccentricity: | 0.0015496 |
| inclination: | 28.4572° |
| perigee height: | 285 km |
| apogee height: | 306 km |
| right ascension of ascending node: | 196.9260° |
| argument of perigee: | 336.8767° |
| revolutions per day: | 15.92441940 |
| mean anomaly at epoch: | 318.3931° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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