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 64866U 26145.38836314 +.00000000 +00000-0 +00000-0 0 00007
2 64866 0.0568 12.9516 0006051 74.1576 272.9596 5.00115909 07
| Epoch (UTC): | 25 May 2026 09:19:14 |
| Eccentricity: | 0.0006051 |
| inclination: | 0.0568° |
| perigee height: | 8057 km |
| apogee height: | 8075 km |
| right ascension of ascending node: | 12.9516° |
| argument of perigee: | 74.1576° |
| revolutions per day: | 5.00115909 |
| mean anomaly at epoch: | 272.9596° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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