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 63818U 25092Q 25201.60078428 .00016595 00000-0 61119-3 0 9996
2 63818 43.0018 42.9135 0001303 269.2672 90.8030 15.27581526 13173
| Epoch (UTC): | 20 July 2025 14:25:07 |
| Eccentricity: | 0.0001303 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 42.9135° |
| argument of perigee: | 269.2672° |
| revolutions per day: | 15.27581526 |
| mean anomaly at epoch: | 90.8030° |
| orbit number at epoch: | 1317 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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