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 64014U 26145.40563189 +.00000000 +00000-0 +69268-3 0 00006
2 64014 42.9931 285.0790 0000238 323.9389 36.1447 15.27599974 09
| Epoch (UTC): | 25 May 2026 09:44:06 |
| Eccentricity: | 0.0000238 |
| inclination: | 42.9931° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 285.0790° |
| argument of perigee: | 323.9389° |
| revolutions per day: | 15.27599974 |
| mean anomaly at epoch: | 36.1447° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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