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 53377U 22096H 24161.83236791 .14771318 26507-5 23601-3 0 9999
2 53377 97.3665 84.2500 0010385 222.5459 137.5041 16.47773285103340
| Epoch (UTC): | 09 June 2024 19:58:36 |
| Eccentricity: | 0.0010385 |
| inclination: | 97.3665° |
| perigee height: | 138 km |
| apogee height: | 152 km |
| right ascension of ascending node: | 84.2500° |
| argument of perigee: | 222.5459° |
| revolutions per day: | 16.47773285 |
| mean anomaly at epoch: | 137.5041° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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