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 64742U 26145.39857657 +.00000000 +00000-0 +31163-3 0 00001
2 64742 53.1578 184.9256 0001143 81.5884 278.5246 15.30206029 04
| Epoch (UTC): | 25 May 2026 09:33:57 |
| Eccentricity: | 0.0001143 |
| inclination: | 53.1578° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 184.9256° |
| argument of perigee: | 81.5884° |
| revolutions per day: | 15.30206029 |
| mean anomaly at epoch: | 278.5246° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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