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 05917U 72022A 23152.41812574 .00000240 00000-0 13123-3 0 9999
2 05917 81.2208 287.9848 0030065 227.7127 132.1494 14.08832515627874
| Epoch (UTC): | 01 June 2023 10:02:06 |
| Eccentricity: | 0.0030065 |
| inclination: | 81.2208° |
| perigee height: | 841 km |
| apogee height: | 885 km |
| right ascension of ascending node: | 287.9848° |
| argument of perigee: | 227.7127° |
| revolutions per day: | 14.08832515 |
| mean anomaly at epoch: | 132.1494° |
| orbit number at epoch: | 62787 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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