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 65224U 26145.33968699 +.00000000 +00000-0 +16217-2 0 00002
2 65224 53.1573 156.1469 0001076 85.2061 274.9065 15.34445535 05
| Epoch (UTC): | 25 May 2026 08:09:08 |
| Eccentricity: | 0.0001076 |
| inclination: | 53.1573° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 156.1469° |
| argument of perigee: | 85.2061° |
| revolutions per day: | 15.34445535 |
| mean anomaly at epoch: | 274.9065° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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