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 21398U 91039B 24258.04905383 .00001576 00000-0 19992-3 0 9990
2 21398 82.5193 282.1512 0021973 143.4134 216.8585 14.80975917795238
| Epoch (UTC): | 14 September 2024 01:10:38 |
| Eccentricity: | 0.0021973 |
| inclination: | 82.5193° |
| perigee height: | 611 km |
| apogee height: | 641 km |
| right ascension of ascending node: | 282.1512° |
| argument of perigee: | 143.4134° |
| revolutions per day: | 14.80975917 |
| mean anomaly at epoch: | 216.8585° |
| orbit number at epoch: | 79523 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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