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 65207U 26145.35231999 +.00000000 +00000-0 +28058-3 0 00008
2 65207 53.1608 156.2264 0001185 77.1120 283.0015 15.34398830 07
| Epoch (UTC): | 25 May 2026 08:27:20 |
| Eccentricity: | 0.0001185 |
| inclination: | 53.1608° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 156.2264° |
| argument of perigee: | 77.1120° |
| revolutions per day: | 15.34398830 |
| mean anomaly at epoch: | 283.0015° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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