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 64290U 26145.48948493 +.00000000 +00000-0 +00000-0 0 00001
2 64290 0.0246 28.9626 0001903 343.0025 291.1649 1.00272242 00
| Epoch (UTC): | 25 May 2026 11:44:51 |
| Eccentricity: | 0.0001903 |
| inclination: | 0.0246° |
| perigee height: | 35778 km |
| apogee height: | 35794 km |
| right ascension of ascending node: | 28.9626° |
| argument of perigee: | 343.0025° |
| revolutions per day: | 1.00272242 |
| mean anomaly at epoch: | 291.1649° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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