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 00020U 59007A 22176.09352480 .00000292 00000-0 10432-3 0 9998
2 00020 33.3530 73.4478 1664676 220.8205 125.5208 11.56227925315977
| Epoch (UTC): | 25 June 2022 02:14:40 |
| Eccentricity: | 0.1664676 |
| inclination: | 33.3530° |
| perigee height: | 508 km |
| apogee height: | 3258 km |
| right ascension of ascending node: | 73.4478° |
| argument of perigee: | 220.8205° |
| revolutions per day: | 11.56227925 |
| mean anomaly at epoch: | 125.5208° |
| orbit number at epoch: | 31597 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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