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 64305U 26145.59960431 +.00000000 +00000-0 +14565-3 0 00000
2 64305 70.0025 0.7453 0002879 268.2064 91.8765 14.98332912 05
| Epoch (UTC): | 25 May 2026 14:23:25 |
| Eccentricity: | 0.0002879 |
| inclination: | 70.0025° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 0.7453° |
| argument of perigee: | 268.2064° |
| revolutions per day: | 14.98332912 |
| mean anomaly at epoch: | 91.8765° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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