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 52017U 22026K 24273.45232859 .15962284 26361-5 29990-3 0 9995
2 52017 97.4545 295.1270 0013084 250.0501 109.9393 16.46521474142074
| Epoch (UTC): | 29 September 2024 10:51:21 |
| Eccentricity: | 0.0013084 |
| inclination: | 97.4545° |
| perigee height: | 140 km |
| apogee height: | 157 km |
| right ascension of ascending node: | 295.1270° |
| argument of perigee: | 250.0501° |
| revolutions per day: | 16.46521474 |
| mean anomaly at epoch: | 109.9393° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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