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 13758U 83001B 22146.38981463 .00000079 00000-0 62421-4 0 9998
2 13758 82.9139 37.1547 0026517 322.2108 37.7188 13.78846902980014
| Epoch (UTC): | 26 May 2022 09:21:19 |
| Eccentricity: | 0.0026517 |
| inclination: | 82.9139° |
| perigee height: | 948 km |
| apogee height: | 987 km |
| right ascension of ascending node: | 37.1547° |
| argument of perigee: | 322.2108° |
| revolutions per day: | 13.78846902 |
| mean anomaly at epoch: | 37.7188° |
| orbit number at epoch: | 98001 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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