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 31165U 99025BHT 24357.02623443 .00014152 00000-0 25525-2 0 9990
2 31165 98.9264 19.6809 0077054 256.4687 133.1836 14.64686187935362
| Epoch (UTC): | 22 December 2024 00:37:46 |
| Eccentricity: | 0.0077054 |
| inclination: | 98.9264° |
| perigee height: | 624 km |
| apogee height: | 732 km |
| right ascension of ascending node: | 19.6809° |
| argument of perigee: | 256.4687° |
| revolutions per day: | 14.64686187 |
| mean anomaly at epoch: | 133.1836° |
| orbit number at epoch: | 93536 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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