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 45875U 20046C 23069.83120406 0.00085000 00000-0 36277-2 0 08
2 45875 53.9765 20.1247 0005409 48.4274 311.5725 15.22388742 05
| Epoch (UTC): | 10 March 2023 19:56:56 |
| Eccentricity: | 0.0005409 |
| inclination: | 53.9765° |
| perigee height: | 495 km |
| apogee height: | 502 km |
| right ascension of ascending node: | 20.1247° |
| argument of perigee: | 48.4274° |
| revolutions per day: | 15.22388742 |
| mean anomaly at epoch: | 311.5725° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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