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 40552U 15020A 23084.47873394 .00000037 00000-0 19835-3 0 9995
2 40552 82.4860 46.0027 0017712 58.0806 302.1991 12.42875159362224
| Epoch (UTC): | 25 March 2023 11:29:22 |
| Eccentricity: | 0.0017712 |
| inclination: | 82.4860° |
| perigee height: | 1480 km |
| apogee height: | 1508 km |
| right ascension of ascending node: | 46.0027° |
| argument of perigee: | 58.0806° |
| revolutions per day: | 12.42875159 |
| mean anomaly at epoch: | 302.1991° |
| orbit number at epoch: | 36222 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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