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 data is extracted from the following two-line orbital elements,
1 41937U 17004A 25131.83844310 -.00000259 00000-0 00000-0 0 9996
2 41937 1.5996 25.3459 0001879 8.7775 284.7823 1.00002961 30571
| Epoch (UTC): | 11 May 2025 20:07:21 |
| Eccentricity: | 0.0001879 |
| inclination: | 1.5996° |
| perigee height: | 35854 km |
| apogee height: | 35869 km |
| right ascension of ascending node: | 25.3459° |
| argument of perigee: | 8.7775° |
| revolutions per day: | 1.00002961 |
| mean anomaly at epoch: | 284.7823° |
| orbit number at epoch: | 3057 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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