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 41937U 26140.59722199 +.00000000 +00000-0 +00000-0 0 00004
2 41937 2.1925 42.5303 0002052 7.8299 63.7927 1.00271602 09
| Epoch (UTC): | 20 May 2026 14:19:59 |
| Eccentricity: | 0.0002052 |
| inclination: | 2.1925° |
| perigee height: | 35778 km |
| apogee height: | 35795 km |
| right ascension of ascending node: | 42.5303° |
| argument of perigee: | 7.8299° |
| revolutions per day: | 1.00271602 |
| mean anomaly at epoch: | 63.7927° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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