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 22274.74045588 .00000580 00000-0 24076-3 0 9996
2 00020 33.3428 81.6865 1664183 24.5487 342.5932 11.56272439327392
| Epoch (UTC): | 01 October 2022 17:46:15 |
| Eccentricity: | 0.1664183 |
| inclination: | 33.3428° |
| perigee height: | 508 km |
| apogee height: | 3257 km |
| right ascension of ascending node: | 81.6865° |
| argument of perigee: | 24.5487° |
| revolutions per day: | 11.56272439 |
| mean anomaly at epoch: | 342.5932° |
| orbit number at epoch: | 32739 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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