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 64760U 26145.54945725 +.00000000 +00000-0 +11461-2 0 00000
2 64760 53.1595 245.4444 0000287 72.3846 287.7187 15.34414888 03
| Epoch (UTC): | 25 May 2026 13:11:13 |
| Eccentricity: | 0.0000287 |
| inclination: | 53.1595° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 245.4444° |
| argument of perigee: | 72.3846° |
| revolutions per day: | 15.34414888 |
| mean anomaly at epoch: | 287.7187° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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