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 65214U 26145.34810388 +.00000000 +00000-0 +81338-4 0 00001
2 65214 53.1598 156.2040 0001426 70.9351 289.1806 15.34409291 09
| Epoch (UTC): | 25 May 2026 08:21:16 |
| Eccentricity: | 0.0001426 |
| inclination: | 53.1598° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 156.2040° |
| argument of perigee: | 70.9351° |
| revolutions per day: | 15.34409291 |
| mean anomaly at epoch: | 289.1806° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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