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 data is extracted from the following two-line orbital elements,
1 22973U 94004 A 94048.00000000 -.00014888 +00000-0 +10000-3 0 9999
2 22973 063.7849 059.2740 9660896 205.9201 046.9616 00.08911390003569
| Epoch (UTC): | 17 February 1994 00:00:00 |
| Eccentricity: | 0.9660896 |
| inclination: | 63.7849° |
| perigee height: | 801 km |
| apogee height: | 409886 km |
| right ascension of ascending node: | 59.2740° |
| argument of perigee: | 205.9201° |
| revolutions per day: | 0.08911390 |
| mean anomaly at epoch: | 46.9616° |
| orbit number at epoch: | 356 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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