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 25682U 99020A 24357.91964448 .00001015 00000-0 21473-3 0 9996
2 25682 97.8738 15.7211 0001664 95.5945 22.4452 14.61239421366690
| Epoch (UTC): | 22 December 2024 22:04:17 |
| Eccentricity: | 0.0001664 |
| inclination: | 97.8738° |
| perigee height: | 688 km |
| apogee height: | 690 km |
| right ascension of ascending node: | 15.7211° |
| argument of perigee: | 95.5945° |
| revolutions per day: | 14.61239421 |
| mean anomaly at epoch: | 22.4452° |
| orbit number at epoch: | 36669 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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