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 62065U 26145.12951602 +.00000000 +00000-0 +77581-3 0 00007
2 62065 53.1564 54.1146 0000884 97.7157 262.3962 15.69727472 02
| Epoch (UTC): | 25 May 2026 03:06:30 |
| Eccentricity: | 0.0000884 |
| inclination: | 53.1564° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 54.1146° |
| argument of perigee: | 97.7157° |
| revolutions per day: | 15.69727472 |
| mean anomaly at epoch: | 262.3962° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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