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 64046U 26145.52756068 +.00000000 +00000-0 +12639-3 0 00004
2 64046 70.0002 280.6364 0002953 271.7252 88.3569 14.98345658 07
| Epoch (UTC): | 25 May 2026 12:39:41 |
| Eccentricity: | 0.0002953 |
| inclination: | 70.0002° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 280.6364° |
| argument of perigee: | 271.7252° |
| revolutions per day: | 14.98345658 |
| mean anomaly at epoch: | 88.3569° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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