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 63816C 25092N 25201.40881944 -.00011132 00000+0 -40314-3 0 2010
2 63816 43.0014 44.6583 0001517 267.9600 199.2543 15.27594070 16
| Epoch (UTC): | 20 July 2025 09:48:42 |
| Eccentricity: | 0.0001517 |
| inclination: | 43.0014° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 44.6583° |
| argument of perigee: | 267.9600° |
| revolutions per day: | 15.27594070 |
| mean anomaly at epoch: | 199.2543° |
| orbit number at epoch: | 1 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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