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 65268U 26145.24291421 +.00000000 +00000-0 +10138-3 0 00009
2 65268 96.5900 76.8468 0003065 185.4488 174.6758 15.96443340 06
| Epoch (UTC): | 25 May 2026 05:49:47 |
| Eccentricity: | 0.0003065 |
| inclination: | 96.5900° |
| perigee height: | 282 km |
| apogee height: | 286 km |
| right ascension of ascending node: | 76.8468° |
| argument of perigee: | 185.4488° |
| revolutions per day: | 15.96443340 |
| mean anomaly at epoch: | 174.6758° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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