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 65956U 26145.02904110 +.00000000 +00000-0 +32716-4 0 00002
2 65956 51.9017 15.4867 0001279 109.7837 250.3264 14.79932477 06
| Epoch (UTC): | 25 May 2026 00:41:49 |
| Eccentricity: | 0.0001279 |
| inclination: | 51.9017° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 15.4867° |
| argument of perigee: | 109.7837° |
| revolutions per day: | 14.79932477 |
| mean anomaly at epoch: | 250.3264° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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