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 64353U 26145.59355410 +.00000000 +00000-0 +24005-3 0 00008
2 64353 70.0010 200.4631 0003782 272.4829 87.5897 14.98331080 02
| Epoch (UTC): | 25 May 2026 14:14:43 |
| Eccentricity: | 0.0003782 |
| inclination: | 70.0010° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 200.4631° |
| argument of perigee: | 272.4829° |
| revolutions per day: | 14.98331080 |
| mean anomaly at epoch: | 87.5897° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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