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 63253U 26145.27686853 +.00000000 +00000-0 +16391-3 0 00008
2 63253 97.6904 37.8152 0001116 331.2168 28.8992 14.97821680 09
| Epoch (UTC): | 25 May 2026 06:38:41 |
| Eccentricity: | 0.0001116 |
| inclination: | 97.6904° |
| perigee height: | 573 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 37.8152° |
| argument of perigee: | 331.2168° |
| revolutions per day: | 14.97821680 |
| mean anomaly at epoch: | 28.8992° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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