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 25034U 97068A 22058.95501692 0.00000000 00000-0 00000-0 0 01
2 25034 63.6025 85.5132 6265301 277.2229 82.7770 2.00654165 06
| Epoch (UTC): | 27 February 2022 22:55:13 |
| Eccentricity: | 0.6265301 |
| inclination: | 63.6025° |
| perigee height: | 3538 km |
| apogee height: | 36810 km |
| right ascension of ascending node: | 85.5132° |
| argument of perigee: | 277.2229° |
| revolutions per day: | 2.00654165 |
| mean anomaly at epoch: | 82.7770° |
| 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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