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 65723U 26145.43407588 +.00000000 +00000-0 +21772-3 0 00005
2 65723 49.9848 53.3453 0009872 134.9697 225.2043 14.83265344 03
| Epoch (UTC): | 25 May 2026 10:25:04 |
| Eccentricity: | 0.0009872 |
| inclination: | 49.9848° |
| perigee height: | 612 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 53.3453° |
| argument of perigee: | 134.9697° |
| revolutions per day: | 14.83265344 |
| mean anomaly at epoch: | 225.2043° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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