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 26038.30954044 +.00000000 +00000-0 +88328-4 0 00005
2 25509 31.4301 134.9903 0336612 9.4985 351.1814 14.33253597 05
| Epoch (UTC): | 07 February 2026 07:25:44 |
| Eccentricity: | 0.0336612 |
| inclination: | 31.4301° |
| perigee height: | 540 km |
| apogee height: | 1022 km |
| right ascension of ascending node: | 134.9903° |
| argument of perigee: | 9.4985° |
| revolutions per day: | 14.33253597 |
| mean anomaly at epoch: | 351.1814° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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