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 23029.35020115 .00002594 00000-0 10562-2 0 9992
2 00020 33.3565 15.0965 1660652 299.8053 44.7545 11.56641215341242
| Epoch (UTC): | 29 January 2023 08:24:17 |
| Eccentricity: | 0.1660652 |
| inclination: | 33.3565° |
| perigee height: | 509 km |
| apogee height: | 3252 km |
| right ascension of ascending node: | 15.0965° |
| argument of perigee: | 299.8053° |
| revolutions per day: | 11.56641215 |
| mean anomaly at epoch: | 44.7545° |
| orbit number at epoch: | 34124 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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