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 26144.80363705 +.00000000 +00000-0 +00000-0 0 00006
2 41937 2.2007 42.6615 0002232 12.5343 137.4089 1.00272479 02
| Epoch (UTC): | 24 May 2026 19:17:14 |
| Eccentricity: | 0.0002232 |
| inclination: | 2.2007° |
| perigee height: | 35777 km |
| apogee height: | 35796 km |
| right ascension of ascending node: | 42.6615° |
| argument of perigee: | 12.5343° |
| revolutions per day: | 1.00272479 |
| mean anomaly at epoch: | 137.4089° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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