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 64302U 26145.48727913 +.00000000 +00000-0 +79643-3 0 00009
2 64302 70.0016 317.8647 0003071 268.0595 92.0235 15.41050513 09
| Epoch (UTC): | 25 May 2026 11:41:40 |
| Eccentricity: | 0.0003071 |
| inclination: | 70.0016° |
| perigee height: | 441 km |
| apogee height: | 445 km |
| right ascension of ascending node: | 317.8647° |
| argument of perigee: | 268.0595° |
| revolutions per day: | 15.41050513 |
| mean anomaly at epoch: | 92.0235° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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