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 26101.51076589 +.00000000 +00000-0 +59107-4 0 00001
2 25338 98.5124 123.9298 0010326 176.2853 183.8407 14.27126056 05
| Epoch (UTC): | 11 April 2026 12:15:30 |
| Eccentricity: | 0.0010326 |
| inclination: | 98.5124° |
| perigee height: | 794 km |
| apogee height: | 809 km |
| right ascension of ascending node: | 123.9298° |
| argument of perigee: | 176.2853° |
| revolutions per day: | 14.27126056 |
| mean anomaly at epoch: | 183.8407° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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