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 65339U 26145.46508509 +.00000000 +00000-0 +33319-3 0 00006
2 65339 53.1588 209.9744 0001071 87.5076 272.6048 15.31711808 09
| Epoch (UTC): | 25 May 2026 11:09:43 |
| Eccentricity: | 0.0001071 |
| inclination: | 53.1588° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 209.9744° |
| argument of perigee: | 87.5076° |
| revolutions per day: | 15.31711808 |
| mean anomaly at epoch: | 272.6048° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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