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 65140U 26145.46421240 +.00000000 +00000-0 +20067-3 0 00008
2 65140 51.8954 173.5660 0000377 27.3627 332.7355 14.79947025 08
| Epoch (UTC): | 25 May 2026 11:08:27 |
| Eccentricity: | 0.0000377 |
| inclination: | 51.8954° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 173.5660° |
| argument of perigee: | 27.3627° |
| revolutions per day: | 14.79947025 |
| mean anomaly at epoch: | 332.7355° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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