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 41783U 26050.86717600 +.00000000 +00000-0 +13195-3 0 00006
2 41783 97.8308 52.9089 0030156 230.7462 129.1067 14.67002752 02
| Epoch (UTC): | 19 February 2026 20:48:44 |
| Eccentricity: | 0.0030156 |
| inclination: | 97.8308° |
| perigee height: | 649 km |
| apogee height: | 692 km |
| right ascension of ascending node: | 52.9089° |
| argument of perigee: | 230.7462° |
| revolutions per day: | 14.67002752 |
| mean anomaly at epoch: | 129.1067° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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