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 is defined by the following mean orbital elements,
1 63413U 26145.40349190 +.00000000 +00000-0 +55771-3 0 00006
2 63413 43.0048 33.6894 0001340 284.0542 76.0161 15.27592014 01
| Epoch (UTC): | 25 May 2026 09:41:01 |
| Eccentricity: | 0.0001340 |
| inclination: | 43.0048° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 33.6894° |
| argument of perigee: | 284.0542° |
| revolutions per day: | 15.27592014 |
| mean anomaly at epoch: | 76.0161° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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