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 52738U 22057G 24334.51223436 .16479580 26697-5 24945-3 0 9995
2 52738 97.5508 111.5244 0009582 276.9617 83.0596 16.48177112140342
| Epoch (UTC): | 29 November 2024 12:17:37 |
| Eccentricity: | 0.0009582 |
| inclination: | 97.5508° |
| perigee height: | 138 km |
| apogee height: | 150 km |
| right ascension of ascending node: | 111.5244° |
| argument of perigee: | 276.9617° |
| revolutions per day: | 16.48177112 |
| mean anomaly at epoch: | 83.0596° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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