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 27433U 02024D 23161.35130965 .00000476 00000-0 27936-3 0 9999
2 27433 99.0504 187.8364 0014900 25.8639 334.3275 14.13022159 85505
| Epoch (UTC): | 10 June 2023 08:25:53 |
| Eccentricity: | 0.0014900 |
| inclination: | 99.0504° |
| perigee height: | 838 km |
| apogee height: | 860 km |
| right ascension of ascending node: | 187.8364° |
| argument of perigee: | 25.8639° |
| revolutions per day: | 14.13022159 |
| mean anomaly at epoch: | 334.3275° |
| orbit number at epoch: | 8550 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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