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 27160U 01049DG 24357.58288495 .00000956 00000-0 16641-3 0 9991
2 27160 98.4066 8.1553 0046853 158.2141 327.3257 14.69838892231464
| Epoch (UTC): | 22 December 2024 13:59:21 |
| Eccentricity: | 0.0046853 |
| inclination: | 98.4066° |
| perigee height: | 628 km |
| apogee height: | 694 km |
| right ascension of ascending node: | 8.1553° |
| argument of perigee: | 158.2141° |
| revolutions per day: | 14.69838892 |
| mean anomaly at epoch: | 327.3257° |
| orbit number at epoch: | 23146 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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