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 64228U 26145.43815049 +.00000000 +00000-0 +46698-3 0 00003
2 64228 53.1593 41.8760 0001799 103.1251 256.9953 15.34404812 06
| Epoch (UTC): | 25 May 2026 10:30:56 |
| Eccentricity: | 0.0001799 |
| inclination: | 53.1593° |
| perigee height: | 461 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 41.8760° |
| argument of perigee: | 103.1251° |
| revolutions per day: | 15.34404812 |
| mean anomaly at epoch: | 256.9953° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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