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 64186U 26145.24535687 +.00000000 +00000-0 +81002-3 0 00000
2 64186 53.1597 95.0071 0001494 85.0968 275.0204 15.31716449 04
| Epoch (UTC): | 25 May 2026 05:53:18 |
| Eccentricity: | 0.0001494 |
| inclination: | 53.1597° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 95.0071° |
| argument of perigee: | 85.0968° |
| revolutions per day: | 15.31716449 |
| mean anomaly at epoch: | 275.0204° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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