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 51092U 97084W 23312.78365133 .00001562 00000-0 61614-3 0 9997
2 51092 45.0271 339.9739 0040282 296.4385 63.2331 14.32566874 88497
| Epoch (UTC): | 08 November 2023 18:48:27 |
| Eccentricity: | 0.0040282 |
| inclination: | 45.0271° |
| perigee height: | 754 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 339.9739° |
| argument of perigee: | 296.4385° |
| revolutions per day: | 14.32566874 |
| mean anomaly at epoch: | 63.2331° |
| orbit number at epoch: | 8849 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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