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 46464U 14055CL 25041.96627491 -.00000013 00000-0 00000-0 0 9990
2 46464 19.4517 200.4013 4923739 66.5983 336.9170 1.82544132 34867
| Epoch (UTC): | 10 February 2025 23:11:26 |
| Eccentricity: | 0.4923739 |
| inclination: | 19.4517° |
| perigee height: | 7978 km |
| apogee height: | 35827 km |
| right ascension of ascending node: | 200.4013° |
| argument of perigee: | 66.5983° |
| revolutions per day: | 1.82544132 |
| mean anomaly at epoch: | 336.9170° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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