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 65262U 26134.84951852 +.00000000 +00000-0 +13643-3 0 00002
2 65262 97.5213 262.3824 0015573 78.2651 282.0838 15.15141877 08
| Epoch (UTC): | 14 May 2026 20:23:18 |
| Eccentricity: | 0.0015573 |
| inclination: | 97.5213° |
| perigee height: | 510 km |
| apogee height: | 531 km |
| right ascension of ascending node: | 262.3824° |
| argument of perigee: | 78.2651° |
| revolutions per day: | 15.15141877 |
| mean anomaly at epoch: | 282.0838° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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