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 4159U 69082AB 23150.83067904 .00000046 00000-0 10012-3 0 9999
2 4159 69.9631 1.2282 0117428 265.2025 93.5651 13.72571975686326
| Epoch (UTC): | 30 May 2023 19:56:10 |
| Eccentricity: | 0.0117428 |
| inclination: | 69.9631° |
| perigee height: | 904 km |
| apogee height: | 1077 km |
| right ascension of ascending node: | 1.2282° |
| argument of perigee: | 265.2025° |
| revolutions per day: | 13.72571975 |
| mean anomaly at epoch: | 93.5651° |
| orbit number at epoch: | 68632 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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