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 25338U 26110.97573951 +.00000000 +00000-0 +47423-4 0 00004
2 25338 98.5112 133.1440 0010874 149.5592 210.6223 14.27128327 03
| Epoch (UTC): | 20 April 2026 23:25:03 |
| Eccentricity: | 0.0010874 |
| inclination: | 98.5112° |
| perigee height: | 794 km |
| apogee height: | 809 km |
| right ascension of ascending node: | 133.1440° |
| argument of perigee: | 149.5592° |
| revolutions per day: | 14.27128327 |
| mean anomaly at epoch: | 210.6223° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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