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 65940U 26145.16194411 +.00000000 +00000-0 +39323-3 0 00005
2 65940 97.6349 225.0962 0012882 212.5821 147.4617 15.15510455 04
| Epoch (UTC): | 25 May 2026 03:53:11 |
| Eccentricity: | 0.0012882 |
| inclination: | 97.6349° |
| perigee height: | 511 km |
| apogee height: | 528 km |
| right ascension of ascending node: | 225.0962° |
| argument of perigee: | 212.5821° |
| revolutions per day: | 15.15510455 |
| mean anomaly at epoch: | 147.4617° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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