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): | 10 November 2024 02:12:17 |
| Eccentricity: | 0.0422319 |
| inclination: | 86.4072° |
| perigee height: | 740 km |
| apogee height: | 1368 km |
| right ascension of ascending node: | 251.6412° |
| argument of perigee: | 302.9794° |
| revolutions per day: | 13.54985939 |
| mean anomaly at epoch: | 53.1420° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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