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 65316U 26145.46185694 +.00000000 +00000-0 +28322-4 0 00006
2 65316 97.1985 222.1017 0002144 102.7180 257.4307 15.40684201 06
| Epoch (UTC): | 25 May 2026 11:05:04 |
| Eccentricity: | 0.0002144 |
| inclination: | 97.1985° |
| perigee height: | 443 km |
| apogee height: | 446 km |
| right ascension of ascending node: | 222.1017° |
| argument of perigee: | 102.7180° |
| revolutions per day: | 15.40684201 |
| mean anomaly at epoch: | 257.4307° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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