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 63800U 26145.51927230 +.00000000 +00000-0 +57910-3 0 00002
2 63800 42.9999 338.5134 0000645 291.2650 68.8133 15.27608775 05
| Epoch (UTC): | 25 May 2026 12:27:45 |
| Eccentricity: | 0.0000645 |
| inclination: | 42.9999° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 338.5134° |
| argument of perigee: | 291.2650° |
| revolutions per day: | 15.27608775 |
| mean anomaly at epoch: | 68.8133° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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