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 65715U 26144.97809406 +.00000000 +00000-0 +20247-3 0 00005
2 65715 49.9836 55.5995 0012955 132.6378 227.5654 14.83274877 07
| Epoch (UTC): | 24 May 2026 23:28:27 |
| Eccentricity: | 0.0012955 |
| inclination: | 49.9836° |
| perigee height: | 610 km |
| apogee height: | 628 km |
| right ascension of ascending node: | 55.5995° |
| argument of perigee: | 132.6378° |
| revolutions per day: | 14.83274877 |
| mean anomaly at epoch: | 227.5654° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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