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 31672U 99025CCE 24257.65825707 .00030825 00000-0 90441-2 0 9992
2 31672 98.9424 53.7060 0129244 260.8641 97.7905 14.38953579582935
| Epoch (UTC): | 13 September 2024 15:47:53 |
| Eccentricity: | 0.0129244 |
| inclination: | 98.9424° |
| perigee height: | 669 km |
| apogee height: | 854 km |
| right ascension of ascending node: | 53.7060° |
| argument of perigee: | 260.8641° |
| revolutions per day: | 14.38953579 |
| mean anomaly at epoch: | 97.7905° |
| orbit number at epoch: | 58293 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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