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 26145.39535051 +.00000000 +00000-0 +48765-4 0 00004
2 41922 86.3951 98.0090 0002541 89.3589 270.7897 14.34217969 08
| Epoch (UTC): | 25 May 2026 09:29:18 |
| Eccentricity: | 0.0002541 |
| inclination: | 86.3951° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 98.0090° |
| argument of perigee: | 89.3589° |
| revolutions per day: | 14.34217969 |
| mean anomaly at epoch: | 270.7897° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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