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 25756U 26106.62804656 +.00000000 +00000-0 +40530-4 0 00006
2 25756 98.6239 140.2055 0014457 91.3043 268.9809 14.55770311 08
| Epoch (UTC): | 16 April 2026 15:04:23 |
| Eccentricity: | 0.0014457 |
| inclination: | 98.6239° |
| perigee height: | 697 km |
| apogee height: | 717 km |
| right ascension of ascending node: | 140.2055° |
| argument of perigee: | 91.3043° |
| revolutions per day: | 14.55770311 |
| mean anomaly at epoch: | 268.9809° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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