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 26356U 00024A 23273.03372097 .00000087 00000-0 00000-0 0 9991
2 26356 12.4239 18.4749 0000784 314.2433 242.2292 1.00278403 22975
| Epoch (UTC): | 30 September 2023 00:48:33 |
| Eccentricity: | 0.0000784 |
| inclination: | 12.4239° |
| perigee height: | 35781 km |
| apogee height: | 35787 km |
| right ascension of ascending node: | 18.4749° |
| argument of perigee: | 314.2433° |
| revolutions per day: | 1.00278403 |
| mean anomaly at epoch: | 242.2292° |
| orbit number at epoch: | 2297 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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