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 30905U 99025AYT 24357.44158022 .00005447 00000-0 28108-2 0 9990
2 30905 98.9051 67.1550 0061140 12.5815 347.6867 14.14505501910938
| Epoch (UTC): | 22 December 2024 10:35:52 |
| Eccentricity: | 0.0061140 |
| inclination: | 98.9051° |
| perigee height: | 800 km |
| apogee height: | 888 km |
| right ascension of ascending node: | 67.1550° |
| argument of perigee: | 12.5815° |
| revolutions per day: | 14.14505501 |
| mean anomaly at epoch: | 347.6867° |
| orbit number at epoch: | 91093 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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