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 41922U 26042.27748078 +.00000000 +00000-0 +45863-4 0 00008
2 41922 86.4022 141.1132 0002539 99.3863 260.7620 14.34218177 03
| Epoch (UTC): | 11 February 2026 06:39:34 |
| Eccentricity: | 0.0002539 |
| inclination: | 86.4022° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 141.1132° |
| argument of perigee: | 99.3863° |
| revolutions per day: | 14.34218177 |
| mean anomaly at epoch: | 260.7620° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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