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 41920U 26145.38266293 +.00000000 +00000-0 +74196-4 0 00007
2 41920 86.3949 97.9721 0002256 85.7500 274.3954 14.34218516 01
| Epoch (UTC): | 25 May 2026 09:11:02 |
| Eccentricity: | 0.0002256 |
| inclination: | 86.3949° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 97.9721° |
| argument of perigee: | 85.7500° |
| revolutions per day: | 14.34218516 |
| mean anomaly at epoch: | 274.3954° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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