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 63829U 26145.36711867 +.00000000 +00000-0 +64587-3 0 00001
2 63829 43.0012 99.3225 0001343 273.0462 87.0236 15.27596892 05
| Epoch (UTC): | 25 May 2026 08:48:39 |
| Eccentricity: | 0.0001343 |
| inclination: | 43.0012° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 99.3225° |
| argument of perigee: | 273.0462° |
| revolutions per day: | 15.27596892 |
| mean anomaly at epoch: | 87.0236° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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