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 64672U 26145.33842222 +.00000000 +00000-0 +63092-3 0 00005
2 64672 53.1599 130.0031 0000481 11.1834 348.9179 15.34430680 03
| Epoch (UTC): | 25 May 2026 08:07:19 |
| Eccentricity: | 0.0000481 |
| inclination: | 53.1599° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 130.0031° |
| argument of perigee: | 11.1834° |
| revolutions per day: | 15.34430680 |
| mean anomaly at epoch: | 348.9179° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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