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 25394U 26110.36278381 +.00000000 +00000-0 +59300-4 0 00005
2 25394 98.9393 82.8455 0000739 345.3020 14.8137 14.25106537 02
| Epoch (UTC): | 20 April 2026 08:42:24 |
| Eccentricity: | 0.0000739 |
| inclination: | 98.9393° |
| perigee height: | 808 km |
| apogee height: | 809 km |
| right ascension of ascending node: | 82.8455° |
| argument of perigee: | 345.3020° |
| revolutions per day: | 14.25106537 |
| mean anomaly at epoch: | 14.8137° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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