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 64142U 26145.30707779 +.00000000 +00000-0 +52322-3 0 00005
2 64142 43.0028 4.9471 0000978 281.1829 78.8913 15.27589674 06
| Epoch (UTC): | 25 May 2026 07:22:11 |
| Eccentricity: | 0.0000978 |
| inclination: | 43.0028° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 4.9471° |
| argument of perigee: | 281.1829° |
| revolutions per day: | 15.27589674 |
| mean anomaly at epoch: | 78.8913° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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