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 64740U 26145.47957810 +.00000000 +00000-0 +71010-3 0 00005
2 64740 53.1584 181.1742 0001248 61.8963 298.2166 15.34394922 07
| Epoch (UTC): | 25 May 2026 11:30:35 |
| Eccentricity: | 0.0001248 |
| inclination: | 53.1584° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 181.1742° |
| argument of perigee: | 61.8963° |
| revolutions per day: | 15.34394922 |
| mean anomaly at epoch: | 298.2166° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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