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 877U 64053B 24279.48154872 .00003068 00000-0 63931-3 0 9995
2 877 65.0797 55.4976 0056390 156.9248 203.4404 14.60603989190791
| Epoch (UTC): | 05 October 2024 11:33:25 |
| Eccentricity: | 0.0056390 |
| inclination: | 65.0797° |
| perigee height: | 651 km |
| apogee height: | 731 km |
| right ascension of ascending node: | 55.4976° |
| argument of perigee: | 156.9248° |
| revolutions per day: | 14.60603989 |
| mean anomaly at epoch: | 203.4404° |
| orbit number at epoch: | 19079 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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