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 53376U 22096G 24129.99598406 .11419415 26171-5 33557-3 0 9995
2 53376 97.3636 52.0981 0009546 227.1141 132.9360 16.44535177 98450
| Epoch (UTC): | 08 May 2024 23:54:13 |
| Eccentricity: | 0.0009546 |
| inclination: | 97.3636° |
| perigee height: | 147 km |
| apogee height: | 160 km |
| right ascension of ascending node: | 52.0981° |
| argument of perigee: | 227.1141° |
| revolutions per day: | 16.44535177 |
| mean anomaly at epoch: | 132.9360° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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