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 40069U 14037A 23265.87695205 .00000192 00000-0 10800-3 0 9998
2 40069 98.4279 267.3297 0006848 63.9082 296.2800 14.20814181477522
| Epoch (UTC): | 22 September 2023 21:02:48 |
| Eccentricity: | 0.0006848 |
| inclination: | 98.4279° |
| perigee height: | 817 km |
| apogee height: | 827 km |
| right ascension of ascending node: | 267.3297° |
| argument of perigee: | 63.9082° |
| revolutions per day: | 14.20814181 |
| mean anomaly at epoch: | 296.2800° |
| orbit number at epoch: | 47752 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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