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 64697U 26145.32541730 +.00000000 +00000-0 +18084-3 0 00002
2 64697 70.0001 121.0859 0003681 266.2918 93.7820 14.98334531 00
| Epoch (UTC): | 25 May 2026 07:48:36 |
| Eccentricity: | 0.0003681 |
| inclination: | 70.0001° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 121.0859° |
| argument of perigee: | 266.2918° |
| revolutions per day: | 14.98334531 |
| mean anomaly at epoch: | 93.7820° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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