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 53385U 22096R 24049.04644770 .13599372 26693-5 33750-3 0 9995
2 53385 97.3603 330.5605 0009443 194.4565 165.6469 16.45419068 86049
| Epoch (UTC): | 18 February 2024 01:06:53 |
| Eccentricity: | 0.0009443 |
| inclination: | 97.3603° |
| perigee height: | 145 km |
| apogee height: | 157 km |
| right ascension of ascending node: | 330.5605° |
| argument of perigee: | 194.4565° |
| revolutions per day: | 16.45419068 |
| mean anomaly at epoch: | 165.6469° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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