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 22279.40616693 .00000873 00000-0 36311-3 0 9995
2 00020 33.3432 65.0447 1664008 49.3307 324.0467 11.56279830327931
| Epoch (UTC): | 06 October 2022 09:44:52 |
| Eccentricity: | 0.1664008 |
| inclination: | 33.3432° |
| perigee height: | 508 km |
| apogee height: | 3257 km |
| right ascension of ascending node: | 65.0447° |
| argument of perigee: | 49.3307° |
| revolutions per day: | 11.56279830 |
| mean anomaly at epoch: | 324.0467° |
| orbit number at epoch: | 32793 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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