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 63399U 26145.40606884 +.00000000 +00000-0 +74603-3 0 00000
2 63399 43.0052 33.7522 0001029 286.5141 73.5597 15.27593397 04
| Epoch (UTC): | 25 May 2026 09:44:44 |
| Eccentricity: | 0.0001029 |
| inclination: | 43.0052° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 33.7522° |
| argument of perigee: | 286.5141° |
| revolutions per day: | 15.27593397 |
| mean anomaly at epoch: | 73.5597° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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