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 64696U 26145.34228142 +.00000000 +00000-0 +20604-3 0 00003
2 64696 70.0000 121.1504 0003257 267.5727 92.5059 14.98336750 03
| Epoch (UTC): | 25 May 2026 08:12:53 |
| Eccentricity: | 0.0003257 |
| inclination: | 70.0000° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 121.1504° |
| argument of perigee: | 267.5727° |
| revolutions per day: | 14.98336750 |
| mean anomaly at epoch: | 92.5059° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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