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 65218U 26145.41114410 +.00000000 +00000-0 +61006-3 0 00005
2 65218 53.1590 155.8815 0001057 88.7794 271.3330 15.34400357 07
| Epoch (UTC): | 25 May 2026 09:52:02 |
| Eccentricity: | 0.0001057 |
| inclination: | 53.1590° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 155.8815° |
| argument of perigee: | 88.7794° |
| revolutions per day: | 15.34400357 |
| mean anomaly at epoch: | 271.3330° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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