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 30281U 99025YS 24357.60616814 .00000649 00000-0 39041-3 0 9991
2 30281 98.7341 351.1450 0029098 161.9635 316.4413 14.10036910922152
| Epoch (UTC): | 22 December 2024 14:32:52 |
| Eccentricity: | 0.0029098 |
| inclination: | 98.7341° |
| perigee height: | 838 km |
| apogee height: | 880 km |
| right ascension of ascending node: | 351.1450° |
| argument of perigee: | 161.9635° |
| revolutions per day: | 14.10036910 |
| mean anomaly at epoch: | 316.4413° |
| orbit number at epoch: | 92215 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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