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 64780U 26145.55778359 +.00000000 +00000-0 +70469-3 0 00004
2 64780 53.1599 244.7774 0000992 290.4713 69.6183 15.34393999 08
| Epoch (UTC): | 25 May 2026 13:23:12 |
| Eccentricity: | 0.0000992 |
| inclination: | 53.1599° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 244.7774° |
| argument of perigee: | 290.4713° |
| revolutions per day: | 15.34393999 |
| mean anomaly at epoch: | 69.6183° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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