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 5917U 72022A 23147.16261027 .00000234 00000-0 12812-3 0 9993
2 5917 81.2201 293.1044 0030105 243.4182 116.3902 14.08829966627419
| Epoch (UTC): | 27 May 2023 03:54:09 |
| Eccentricity: | 0.0030105 |
| inclination: | 81.2201° |
| perigee height: | 841 km |
| apogee height: | 885 km |
| right ascension of ascending node: | 293.1044° |
| argument of perigee: | 243.4182° |
| revolutions per day: | 14.08829966 |
| mean anomaly at epoch: | 116.3902° |
| orbit number at epoch: | 62741 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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