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 21224U 91027 A 91101.02620370 .00009953 +00000-0 +25600-3 0 9994
2 21224 028.4742 201.2870 0012157 343.1172 318.8032 15.37291117000830
| Epoch (UTC): | 11 April 1991 00:37:44 |
| Eccentricity: | 0.0012157 |
| inclination: | 28.4742° |
| perigee height: | 446 km |
| apogee height: | 462 km |
| right ascension of ascending node: | 201.2870° |
| argument of perigee: | 343.1172° |
| revolutions per day: | 15.37291117 |
| mean anomaly at epoch: | 318.8032° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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