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 26545U 00057A 23083.60353191 .00005026 00000-0 56960-3 0 9990
2 26545 64.5571 29.3213 0051479 291.3767 68.1852 14.86497543217150
| Epoch (UTC): | 24 March 2023 14:29:05 |
| Eccentricity: | 0.0051479 |
| inclination: | 64.5571° |
| perigee height: | 573 km |
| apogee height: | 645 km |
| right ascension of ascending node: | 29.3213° |
| argument of perigee: | 291.3767° |
| revolutions per day: | 14.86497543 |
| mean anomaly at epoch: | 68.1852° |
| orbit number at epoch: | 21715 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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