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 63302U 26145.49940044 +.00000000 +00000-0 +22929-3 0 00006
2 63302 97.8986 270.2588 0003616 68.6804 291.4789 14.72326675 06
| Epoch (UTC): | 25 May 2026 11:59:08 |
| Eccentricity: | 0.0003616 |
| inclination: | 97.8986° |
| perigee height: | 651 km |
| apogee height: | 656 km |
| right ascension of ascending node: | 270.2588° |
| argument of perigee: | 68.6804° |
| revolutions per day: | 14.72326675 |
| mean anomaly at epoch: | 291.4789° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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