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 115U 60002D 22187.58058564 .00000551 00000-0 90699-4 0 9994
2 115 48.1668 270.4952 0034543 310.7388 49.0527 14.84437333324220
| Epoch (UTC): | 06 July 2022 13:56:02 |
| Eccentricity: | 0.0034543 |
| inclination: | 48.1668° |
| perigee height: | 591 km |
| apogee height: | 639 km |
| right ascension of ascending node: | 270.4952° |
| argument of perigee: | 310.7388° |
| revolutions per day: | 14.84437333 |
| mean anomaly at epoch: | 49.0527° |
| orbit number at epoch: | 32422 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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