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 65722U 26145.15750794 +.00000000 +00000-0 +19590-3 0 00008
2 65722 49.9910 55.4109 0011658 144.1575 216.0148 14.83278115 00
| Epoch (UTC): | 25 May 2026 03:46:48 |
| Eccentricity: | 0.0011658 |
| inclination: | 49.9910° |
| perigee height: | 611 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 55.4109° |
| argument of perigee: | 144.1575° |
| revolutions per day: | 14.83278115 |
| mean anomaly at epoch: | 216.0148° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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