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 64554U 26109.29775485 +.00000000 +00000-0 +60683-3 0 00008
2 64554 97.4575 226.2183 0002465 141.1882 218.9535 15.28608137 03
| Epoch (UTC): | 19 April 2026 07:08:46 |
| Eccentricity: | 0.0002465 |
| inclination: | 97.4575° |
| perigee height: | 478 km |
| apogee height: | 482 km |
| right ascension of ascending node: | 226.2183° |
| argument of perigee: | 141.1882° |
| revolutions per day: | 15.28608137 |
| mean anomaly at epoch: | 218.9535° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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