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 23151.84996218 .00000240 00000-0 13127-3 0 9997
2 05917 81.2208 288.5382 0030067 229.4089 130.4465 14.08832225627790
| Epoch (UTC): | 31 May 2023 20:23:56 |
| Eccentricity: | 0.0030067 |
| inclination: | 81.2208° |
| perigee height: | 841 km |
| apogee height: | 885 km |
| right ascension of ascending node: | 288.5382° |
| argument of perigee: | 229.4089° |
| revolutions per day: | 14.08832225 |
| mean anomaly at epoch: | 130.4465° |
| orbit number at epoch: | 62779 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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