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 25396U 26087.89457507 +.00000000 +00000-0 +10083-3 0 00001
2 25396 98.9836 76.9858 0003381 49.3189 310.8283 14.25733177 07
| Epoch (UTC): | 28 March 2026 21:28:11 |
| Eccentricity: | 0.0003381 |
| inclination: | 98.9836° |
| perigee height: | 804 km |
| apogee height: | 808 km |
| right ascension of ascending node: | 76.9858° |
| argument of perigee: | 49.3189° |
| revolutions per day: | 14.25733177 |
| mean anomaly at epoch: | 310.8283° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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