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 39441U 26107.55964328 +.00000000 +00000-0 +13939-3 0 00000
2 39441 97.8861 47.2306 0064815 268.6239 90.7551 14.86401792 03
| Epoch (UTC): | 17 April 2026 13:25:53 |
| Eccentricity: | 0.0064815 |
| inclination: | 97.8861° |
| perigee height: | 564 km |
| apogee height: | 654 km |
| right ascension of ascending node: | 47.2306° |
| argument of perigee: | 268.6239° |
| revolutions per day: | 14.86401792 |
| mean anomaly at epoch: | 90.7551° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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