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 64717U 26145.35463478 +.00000000 +00000-0 +30369-3 0 00000
2 64717 70.0001 121.1889 0003822 266.6623 93.4099 14.98339705 04
| Epoch (UTC): | 25 May 2026 08:30:40 |
| Eccentricity: | 0.0003822 |
| inclination: | 70.0001° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 121.1889° |
| argument of perigee: | 266.6623° |
| revolutions per day: | 14.98339705 |
| mean anomaly at epoch: | 93.4099° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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