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 62715U 26145.46773176 +.00000000 +00000-0 +53657-4 0 00003
2 62715 97.7083 224.6472 0000197 121.1866 238.9373 14.94126909 06
| Epoch (UTC): | 25 May 2026 11:13:32 |
| Eccentricity: | 0.0000197 |
| inclination: | 97.7083° |
| perigee height: | 585 km |
| apogee height: | 585 km |
| right ascension of ascending node: | 224.6472° |
| argument of perigee: | 121.1866° |
| revolutions per day: | 14.94126909 |
| mean anomaly at epoch: | 238.9373° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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