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 65406U 26145.24172353 +.00000000 +00000-0 +47265-3 0 00006
2 65406 53.1573 236.8487 0001221 87.4355 272.6786 15.30210377 00
| Epoch (UTC): | 25 May 2026 05:48:04 |
| Eccentricity: | 0.0001221 |
| inclination: | 53.1573° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 236.8487° |
| argument of perigee: | 87.4355° |
| revolutions per day: | 15.30210377 |
| mean anomaly at epoch: | 272.6786° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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