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 20624U 90046A 23272.82281122 .00000356 00000-0 20994-3 0 9996
2 20624 71.0382 88.8347 0013392 130.7206 229.5082 14.14490700721493
| Epoch (UTC): | 29 September 2023 19:44:50 |
| Eccentricity: | 0.0013392 |
| inclination: | 71.0382° |
| perigee height: | 834 km |
| apogee height: | 854 km |
| right ascension of ascending node: | 88.8347° |
| argument of perigee: | 130.7206° |
| revolutions per day: | 14.14490700 |
| mean anomaly at epoch: | 229.5082° |
| orbit number at epoch: | 72149 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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