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 26040.32396259 +.00000000 +00000-0 +60494-4 0 00009
2 41922 86.4021 141.9282 0002460 99.4213 260.7261 14.34217625 07
| Epoch (UTC): | 09 February 2026 07:46:30 |
| Eccentricity: | 0.0002460 |
| inclination: | 86.4021° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 141.9282° |
| argument of perigee: | 99.4213° |
| revolutions per day: | 14.34217625 |
| mean anomaly at epoch: | 260.7261° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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