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 26072.55482542 +.00000000 +00000-0 +92097-4 0 00007
2 25338 98.5159 95.7352 0009049 267.2833 92.7313 14.27114334 09
| Epoch (UTC): | 13 March 2026 13:18:56 |
| Eccentricity: | 0.0009049 |
| inclination: | 98.5159° |
| perigee height: | 795 km |
| apogee height: | 808 km |
| right ascension of ascending node: | 95.7352° |
| argument of perigee: | 267.2833° |
| revolutions per day: | 14.27114334 |
| mean anomaly at epoch: | 92.7313° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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