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 53240U 22085B 22211.66485537 .27550885 82783-5 14714-3 0 9996
2 53240 41.4657 310.5880 0016171 234.0115 268.0618 16.53851699 1038
| Epoch (UTC): | 30 July 2022 15:57:23 |
| Eccentricity: | 0.0016171 |
| inclination: | 41.4657° |
| perigee height: | 118 km |
| apogee height: | 140 km |
| right ascension of ascending node: | 310.5880° |
| argument of perigee: | 234.0115° |
| revolutions per day: | 16.53851699 |
| mean anomaly at epoch: | 268.0618° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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