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 24256.74645230 .00009251 00000-0 36976-2 0 9993
2 20 33.3506 56.2349 1648683 214.9312 133.1342 11.59710494409967
| Epoch (UTC): | 12 September 2024 17:54:53 |
| Eccentricity: | 0.1648683 |
| inclination: | 33.3506° |
| perigee height: | 507 km |
| apogee height: | 3225 km |
| right ascension of ascending node: | 56.2349° |
| argument of perigee: | 214.9312° |
| revolutions per day: | 11.59710494 |
| mean anomaly at epoch: | 133.1342° |
| orbit number at epoch: | 40996 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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