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 62041U 26145.45938480 +.00000000 +00000-0 +74063-3 0 00008
2 62041 42.9997 183.0176 0001817 272.9280 87.1364 15.27581192 08
| Epoch (UTC): | 25 May 2026 11:01:30 |
| Eccentricity: | 0.0001817 |
| inclination: | 42.9997° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 183.0176° |
| argument of perigee: | 272.9280° |
| revolutions per day: | 15.27581192 |
| mean anomaly at epoch: | 87.1364° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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