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 63263U 26145.62944345 +.00000000 +00000-0 +21308-3 0 00005
2 63263 97.6882 38.3353 0003359 68.7384 291.4197 14.96656156 05
| Epoch (UTC): | 25 May 2026 15:06:23 |
| Eccentricity: | 0.0003359 |
| inclination: | 97.6882° |
| perigee height: | 575 km |
| apogee height: | 580 km |
| right ascension of ascending node: | 38.3353° |
| argument of perigee: | 68.7384° |
| revolutions per day: | 14.96656156 |
| mean anomaly at epoch: | 291.4197° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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