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 65359U 26145.34000727 +.00000000 +00000-0 +60507-3 0 00003
2 65359 53.1595 171.9354 0001067 77.0276 283.0844 15.30212687 05
| Epoch (UTC): | 25 May 2026 08:09:36 |
| Eccentricity: | 0.0001067 |
| inclination: | 53.1595° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 171.9354° |
| argument of perigee: | 77.0276° |
| revolutions per day: | 15.30212687 |
| mean anomaly at epoch: | 283.0844° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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