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 20U 59007A 23029.26383417 .00002626 00000-0 10696-2 0 9993
2 20 33.3565 15.4048 1660652 299.3466 45.1304 11.56640855341260
| Epoch (UTC): | 29 January 2023 06:19:55 |
| Eccentricity: | 0.1660652 |
| inclination: | 33.3565° |
| perigee height: | 509 km |
| apogee height: | 3252 km |
| right ascension of ascending node: | 15.4048° |
| argument of perigee: | 299.3466° |
| revolutions per day: | 11.56640855 |
| mean anomaly at epoch: | 45.1304° |
| orbit number at epoch: | 34126 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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