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 64699U 26145.36715411 +.00000000 +00000-0 +19959-3 0 00009
2 64699 70.0011 121.2073 0004193 262.9251 97.1431 14.98342013 05
| Epoch (UTC): | 25 May 2026 08:48:42 |
| Eccentricity: | 0.0004193 |
| inclination: | 70.0011° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 121.2073° |
| argument of perigee: | 262.9251° |
| revolutions per day: | 14.98342013 |
| mean anomaly at epoch: | 97.1431° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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