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 27430U 02024A 24357.84647237 .00000741 00000-0 28982-3 0 9990
2 27430 98.6556 307.1635 0007823 227.5553 132.4969 14.32522410180480
| Epoch (UTC): | 22 December 2024 20:18:55 |
| Eccentricity: | 0.0007823 |
| inclination: | 98.6556° |
| perigee height: | 778 km |
| apogee height: | 789 km |
| right ascension of ascending node: | 307.1635° |
| argument of perigee: | 227.5553° |
| revolutions per day: | 14.32522410 |
| mean anomaly at epoch: | 132.4969° |
| orbit number at epoch: | 18048 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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