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 22251U 92083A 00144.08477388 .00006500 00000-0 39753-3 0 02
2 22251 97.7220 176.9518 0371000 43.9370 316.0628 14.67328193 05
| Epoch (UTC): | 23 May 2000 02:02:04 |
| Eccentricity: | 0.0371000 |
| inclination: | 97.7220° |
| perigee height: | 408 km |
| apogee height: | 931 km |
| right ascension of ascending node: | 176.9518° |
| argument of perigee: | 43.9370° |
| revolutions per day: | 14.67328193 |
| mean anomaly at epoch: | 316.0628° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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