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 09482U 26039.22838110 +.00000000 +00000-0 +57953-4 0 00004
2 09482 81.2565 294.8176 0082467 248.8451 110.3892 14.07972269 09
| Epoch (UTC): | 08 February 2026 05:28:52 |
| Eccentricity: | 0.0082467 |
| inclination: | 81.2565° |
| perigee height: | 807 km |
| apogee height: | 926 km |
| right ascension of ascending node: | 294.8176° |
| argument of perigee: | 248.8451° |
| revolutions per day: | 14.07972269 |
| mean anomaly at epoch: | 110.3892° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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