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 25338U 98030A 24259.92022783 .00000789 00000-0 34383-3 0 9994
2 25338 98.5646 285.1389 0011304 63.2670 296.9666 14.26709834370121
| Epoch (UTC): | 15 September 2024 22:05:07 |
| Eccentricity: | 0.0011304 |
| inclination: | 98.5646° |
| perigee height: | 794 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 285.1389° |
| argument of perigee: | 63.2670° |
| revolutions per day: | 14.26709834 |
| mean anomaly at epoch: | 296.9666° |
| orbit number at epoch: | 37012 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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