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 28904U 05046C 23333.26666861 .00000394 00000-0 11660-2 0 9995
2 28904 6.8933 116.7618 7211491 321.2430 4.5765 2.29444050150872
| Epoch (UTC): | 29 November 2023 06:24:00 |
| Eccentricity: | 0.7211491 |
| inclination: | 6.8933° |
| perigee height: | 393 km |
| apogee height: | 35414 km |
| right ascension of ascending node: | 116.7618° |
| argument of perigee: | 321.2430° |
| revolutions per day: | 2.29444050 |
| mean anomaly at epoch: | 4.5765° |
| orbit number at epoch: | 15087 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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