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 64373U 26145.60166561 +.00000000 +00000-0 +12358-2 0 00006
2 64373 43.0000 341.3816 0001570 229.6378 130.4352 15.70795018 09
| Epoch (UTC): | 25 May 2026 14:26:23 |
| Eccentricity: | 0.0001570 |
| inclination: | 43.0000° |
| perigee height: | 356 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 341.3816° |
| argument of perigee: | 229.6378° |
| revolutions per day: | 15.70795018 |
| mean anomaly at epoch: | 130.4352° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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