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 63257U 26145.65701366 +.00000000 +00000-0 +32457-3 0 00002
2 63257 97.7511 40.8063 0002030 58.2523 301.8898 15.00928515 09
| Epoch (UTC): | 25 May 2026 15:46:05 |
| Eccentricity: | 0.0002030 |
| inclination: | 97.7511° |
| perigee height: | 563 km |
| apogee height: | 565 km |
| right ascension of ascending node: | 40.8063° |
| argument of perigee: | 58.2523° |
| revolutions per day: | 15.00928515 |
| mean anomaly at epoch: | 301.8898° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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