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 45876U 20046D 23073.79575234 0.00128000 00000-0 51918-2 0 09
2 45876 53.9670 2.4862 0000264 308.9066 50.7384 15.24118401 02
| Epoch (UTC): | 14 March 2023 19:05:53 |
| Eccentricity: | 0.0000264 |
| inclination: | 53.9670° |
| perigee height: | 493 km |
| apogee height: | 493 km |
| right ascension of ascending node: | 2.4862° |
| argument of perigee: | 308.9066° |
| revolutions per day: | 15.24118401 |
| mean anomaly at epoch: | 50.7384° |
| 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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