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 63279U 26145.44105729 +.00000000 +00000-0 +64510-3 0 00009
2 63279 43.0048 164.6848 0002863 255.4846 104.5688 15.27590912 01
| Epoch (UTC): | 25 May 2026 10:35:07 |
| Eccentricity: | 0.0002863 |
| inclination: | 43.0048° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 164.6848° |
| argument of perigee: | 255.4846° |
| revolutions per day: | 15.27590912 |
| mean anomaly at epoch: | 104.5688° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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