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 24284.56338523 .00003997 00000-0 16099-2 0 9993
2 00020 33.3450 316.4615 1647184 3.4568 357.5971 11.59917603413169
| Epoch (UTC): | 10 October 2024 13:31:16 |
| Eccentricity: | 0.1647184 |
| inclination: | 33.3450° |
| perigee height: | 507 km |
| apogee height: | 3223 km |
| right ascension of ascending node: | 316.4615° |
| argument of perigee: | 3.4568° |
| revolutions per day: | 11.59917603 |
| mean anomaly at epoch: | 357.5971° |
| orbit number at epoch: | 41316 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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