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 65338U 26145.59091802 +.00000000 +00000-0 +44161-3 0 00009
2 65338 53.1586 209.3350 0001065 83.5364 276.5759 15.31716188 00
| Epoch (UTC): | 25 May 2026 14:10:55 |
| Eccentricity: | 0.0001065 |
| inclination: | 53.1586° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 209.3350° |
| argument of perigee: | 83.5364° |
| revolutions per day: | 15.31716188 |
| mean anomaly at epoch: | 276.5759° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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