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 25568U 26088.20372058 +.00000000 +00000-0 +11877-3 0 00007
2 25568 82.9494 142.8729 0023445 309.7372 114.3400 13.73127684 01
| Epoch (UTC): | 29 March 2026 04:53:21 |
| Eccentricity: | 0.0023445 |
| inclination: | 82.9494° |
| perigee height: | 971 km |
| apogee height: | 1006 km |
| right ascension of ascending node: | 142.8729° |
| argument of perigee: | 309.7372° |
| revolutions per day: | 13.73127684 |
| mean anomaly at epoch: | 114.3400° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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