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 41789U 26053.76686161 +.00000000 +00000-0 +15173-3 0 00009
2 41789 97.8026 62.2223 0025519 190.8900 169.1757 14.69076808 04
| Epoch (UTC): | 22 February 2026 18:24:16 |
| Eccentricity: | 0.0025519 |
| inclination: | 97.8026° |
| perigee height: | 646 km |
| apogee height: | 682 km |
| right ascension of ascending node: | 62.2223° |
| argument of perigee: | 190.8900° |
| revolutions per day: | 14.69076808 |
| mean anomaly at epoch: | 169.1757° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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