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 63261U 26145.46402912 +.00000000 +00000-0 +33070-3 0 00003
2 63261 97.6949 39.0782 0003731 96.9514 263.2133 14.98899283 02
| Epoch (UTC): | 25 May 2026 11:08:12 |
| Eccentricity: | 0.0003731 |
| inclination: | 97.6949° |
| perigee height: | 568 km |
| apogee height: | 573 km |
| right ascension of ascending node: | 39.0782° |
| argument of perigee: | 96.9514° |
| revolutions per day: | 14.98899283 |
| mean anomaly at epoch: | 263.2133° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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