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 63799U 26145.52312557 +.00000000 +00000-0 +39437-3 0 00004
2 63799 42.9986 338.5412 0000785 255.9309 104.1456 15.27594238 00
| Epoch (UTC): | 25 May 2026 12:33:18 |
| Eccentricity: | 0.0000785 |
| inclination: | 42.9986° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 338.5412° |
| argument of perigee: | 255.9309° |
| revolutions per day: | 15.27594238 |
| mean anomaly at epoch: | 104.1456° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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