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,
| Epoch (UTC): | 16 July 2025 21:06:39 |
| Eccentricity: | 0.4946527 |
| inclination: | 38.9537° |
| perigee height: | 53076 km |
| apogee height: | 169467 km |
| right ascension of ascending node: | 15.4074° |
| argument of perigee: | 279.1044° |
| revolutions per day: | 0.21513482 |
| mean anomaly at epoch: | 359.3388° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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