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 64131U 26145.51263985 +.00000000 +00000-0 +11734-2 0 00003
2 64131 43.0013 230.5796 0002826 262.0613 97.9934 15.70900061 08
| Epoch (UTC): | 25 May 2026 12:18:12 |
| Eccentricity: | 0.0002826 |
| inclination: | 43.0013° |
| perigee height: | 354 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 230.5796° |
| argument of perigee: | 262.0613° |
| revolutions per day: | 15.70900061 |
| mean anomaly at epoch: | 97.9934° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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