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 25509U 26106.35785002 +.00000000 +00000-0 +63485-4 0 00009
2 25509 31.4315 107.1288 0336561 249.2774 107.1472 14.33308602 08
| Epoch (UTC): | 16 April 2026 08:35:18 |
| Eccentricity: | 0.0336561 |
| inclination: | 31.4315° |
| perigee height: | 540 km |
| apogee height: | 1022 km |
| right ascension of ascending node: | 107.1288° |
| argument of perigee: | 249.2774° |
| revolutions per day: | 14.33308602 |
| mean anomaly at epoch: | 107.1472° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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