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 64130U 26145.59215029 +.00000000 +00000-0 +12367-2 0 00009
2 64130 43.0030 230.3239 0002139 267.8777 92.1846 15.70860592 00
| Epoch (UTC): | 25 May 2026 14:12:41 |
| Eccentricity: | 0.0002139 |
| inclination: | 43.0030° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 230.3239° |
| argument of perigee: | 267.8777° |
| revolutions per day: | 15.70860592 |
| mean anomaly at epoch: | 92.1846° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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