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 65270U 26145.46231758 +.00000000 +00000-0 +48089-5 0 00001
2 65270 96.5883 77.0231 0004923 163.5207 196.6232 15.96145566 00
| Epoch (UTC): | 25 May 2026 11:05:44 |
| Eccentricity: | 0.0004923 |
| inclination: | 96.5883° |
| perigee height: | 282 km |
| apogee height: | 288 km |
| right ascension of ascending node: | 77.0231° |
| argument of perigee: | 163.5207° |
| revolutions per day: | 15.96145566 |
| mean anomaly at epoch: | 196.6232° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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