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 20242U 89075 A 89271.91910735 .00392374 -10700-4 +11056-3 00359
2 20242 082.3202 102.1072 0028181 060.2745 300.1368 16.26505095002211
| Epoch (UTC): | 28 September 1989 22:03:30 |
| Eccentricity: | 0.0028181 |
| inclination: | 82.3202° |
| perigee height: | 183 km |
| apogee height: | 220 km |
| right ascension of ascending node: | 102.1072° |
| argument of perigee: | 60.2745° |
| revolutions per day: | 16.26505095 |
| mean anomaly at epoch: | 300.1368° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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