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 65682U 26145.25498402 +.00000000 +00000-0 +10111-2 0 00008
2 65682 53.1594 348.7871 0002118 67.7255 292.3972 15.34402363 03
| Epoch (UTC): | 25 May 2026 06:07:10 |
| Eccentricity: | 0.0002118 |
| inclination: | 53.1594° |
| perigee height: | 461 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 348.7871° |
| argument of perigee: | 67.7255° |
| revolutions per day: | 15.34402363 |
| mean anomaly at epoch: | 292.3972° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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