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 65719U 26145.17230060 +.00000000 +00000-0 +21399-3 0 00005
2 65719 49.9816 54.5680 0009650 145.1193 215.0379 14.83274754 01
| Epoch (UTC): | 25 May 2026 04:08:06 |
| Eccentricity: | 0.0009650 |
| inclination: | 49.9816° |
| perigee height: | 612 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 54.5680° |
| argument of perigee: | 145.1193° |
| revolutions per day: | 14.83274754 |
| mean anomaly at epoch: | 215.0379° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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