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 23646U 95039F 97099.00000000 -.00001302 +00000-0 +10000-3 0 9992
2 23646 070.3422 248.3458 7715642 328.5234 102.6257 00.26402863001616
| Epoch (UTC): | 09 April 1997 00:00:00 |
| Eccentricity: | 0.7715642 |
| inclination: | 70.3422° |
| perigee height: | 17067 km |
| apogee height: | 175447 km |
| right ascension of ascending node: | 248.3458° |
| argument of perigee: | 328.5234° |
| revolutions per day: | 0.26402863 |
| mean anomaly at epoch: | 102.6257° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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