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 23150.90165036 -.00000079 00000-0 -40105-3 0 9990
2 29528 51.4132 351.4852 5996926 138.1678 293.7547 3.64268770220310
| Epoch (UTC): | 30 May 2023 21:38:22 |
| Eccentricity: | 0.5996926 |
| inclination: | 51.4132° |
| perigee height: | 764 km |
| apogee height: | 22164 km |
| right ascension of ascending node: | 351.4852° |
| argument of perigee: | 138.1678° |
| revolutions per day: | 3.64268770 |
| mean anomaly at epoch: | 293.7547° |
| orbit number at epoch: | 22031 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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