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 31688U 99025CCW 24280.91300826 .00000724 00000-0 49247-3 0 9998
2 31688 99.0281 334.6624 0073676 259.5079 99.7779 14.02005104892959
| Epoch (UTC): | 06 October 2024 21:54:43 |
| Eccentricity: | 0.0073676 |
| inclination: | 99.0281° |
| perigee height: | 833 km |
| apogee height: | 940 km |
| right ascension of ascending node: | 334.6624° |
| argument of perigee: | 259.5079° |
| revolutions per day: | 14.02005104 |
| mean anomaly at epoch: | 99.7779° |
| orbit number at epoch: | 89295 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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