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 64707U 26145.34211407 +.00000000 +00000-0 +25982-3 0 00006
2 64707 69.9999 121.1443 0004367 261.7997 98.2667 14.98335488 05
| Epoch (UTC): | 25 May 2026 08:12:38 |
| Eccentricity: | 0.0004367 |
| inclination: | 69.9999° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 121.1443° |
| argument of perigee: | 261.7997° |
| revolutions per day: | 14.98335488 |
| mean anomaly at epoch: | 98.2667° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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