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 22U 59009A 25134.75464578 .00006807 00000-0 30450-3 0 9994
2 22 50.2763 253.9018 0093027 330.8214 28.7564 15.18614932494569
| Epoch (UTC): | 14 May 2025 18:06:41 |
| Eccentricity: | 0.0093027 |
| inclination: | 50.2763° |
| perigee height: | 446 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 253.9018° |
| argument of perigee: | 330.8214° |
| revolutions per day: | 15.18614932 |
| mean anomaly at epoch: | 28.7564° |
| orbit number at epoch: | 49456 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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