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 23271.91043003 .00001071 00000-0 43322-3 0 9994
2 00020 33.3405 228.4084 1656331 150.3631 220.2084 11.57842272369357
| Epoch (UTC): | 28 September 2023 21:51:01 |
| Eccentricity: | 0.1656331 |
| inclination: | 33.3405° |
| perigee height: | 508 km |
| apogee height: | 3242 km |
| right ascension of ascending node: | 228.4084° |
| argument of perigee: | 150.3631° |
| revolutions per day: | 11.57842272 |
| mean anomaly at epoch: | 220.2084° |
| orbit number at epoch: | 36935 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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