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 25042U 26088.04314168 +.00000000 +00000-0 +19321-3 0 00006
2 25042 86.3849 88.9998 0019879 76.3601 283.9815 14.49677406 05
| Epoch (UTC): | 29 March 2026 01:02:07 |
| Eccentricity: | 0.0019879 |
| inclination: | 86.3849° |
| perigee height: | 713 km |
| apogee height: | 741 km |
| right ascension of ascending node: | 88.9998° |
| argument of perigee: | 76.3601° |
| revolutions per day: | 14.49677406 |
| mean anomaly at epoch: | 283.9815° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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