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 25544U 98067A 23266.21694471 .00015563 00000-0 28444-3 0 9998
2 25544 51.6419 202.9636 0005914 50.3182 96.1908 15.49552217416997
| Epoch (UTC): | 23 September 2023 05:12:24 |
| Eccentricity: | 0.0005914 |
| inclination: | 51.6419° |
| perigee height: | 414 km |
| apogee height: | 422 km |
| right ascension of ascending node: | 202.9636° |
| argument of perigee: | 50.3182° |
| revolutions per day: | 15.49552217 |
| mean anomaly at epoch: | 96.1908° |
| orbit number at epoch: | 41699 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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