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 63817U 26145.34913009 +.00000000 +00000-0 +55694-3 0 00007
2 63817 43.0006 99.1882 0001556 268.6478 91.4195 15.27593592 02
| Epoch (UTC): | 25 May 2026 08:22:44 |
| Eccentricity: | 0.0001556 |
| inclination: | 43.0006° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 99.1882° |
| argument of perigee: | 268.6478° |
| revolutions per day: | 15.27593592 |
| mean anomaly at epoch: | 91.4195° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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