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 52950U 22074G 23337.71084856 .08632586 10495-4 13694-2 0 9999
2 52950 44.9882 107.4898 0009862 322.2340 37.7890 16.32664942 80078
| Epoch (UTC): | 03 December 2023 17:03:37 |
| Eccentricity: | 0.0009862 |
| inclination: | 44.9882° |
| perigee height: | 179 km |
| apogee height: | 192 km |
| right ascension of ascending node: | 107.4898° |
| argument of perigee: | 322.2340° |
| revolutions per day: | 16.32664942 |
| mean anomaly at epoch: | 37.7890° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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