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 64701U 26145.32977359 +.00000000 +00000-0 +40945-3 0 00009
2 64701 69.9999 121.0718 0003620 261.2797 98.7952 14.98342298 06
| Epoch (UTC): | 25 May 2026 07:54:52 |
| Eccentricity: | 0.0003620 |
| inclination: | 69.9999° |
| perigee height: | 570 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 121.0718° |
| argument of perigee: | 261.2797° |
| revolutions per day: | 14.98342298 |
| mean anomaly at epoch: | 98.7952° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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