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 64385U 26145.25604115 +.00000000 +00000-0 +35827-3 0 00009
2 64385 42.9987 107.6582 0000896 252.1950 107.8804 15.27581076 03
| Epoch (UTC): | 25 May 2026 06:08:41 |
| Eccentricity: | 0.0000896 |
| inclination: | 42.9987° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 107.6582° |
| argument of perigee: | 252.1950° |
| revolutions per day: | 15.27581076 |
| mean anomaly at epoch: | 107.8804° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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