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 data is extracted from the following two-line orbital elements,
1 29528U 06051C 23149.84724743 -.00000066 00000-0 -27790-3 0 9998
2 29528 51.4126 351.9227 5996946 137.8352 351.0489 3.64268803220287
| Epoch (UTC): | 29 May 2023 20:20:02 |
| Eccentricity: | 0.5996946 |
| inclination: | 51.4126° |
| perigee height: | 764 km |
| apogee height: | 22164 km |
| right ascension of ascending node: | 351.9227° |
| argument of perigee: | 137.8352° |
| revolutions per day: | 3.64268803 |
| mean anomaly at epoch: | 351.0489° |
| orbit number at epoch: | 22028 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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