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 04589U 70086B 24287.48341005 .00001600 00000-0 48763-3 0 9993
2 04589 74.0611 48.0314 0021309 306.9442 52.9762 14.42685219832286
| Epoch (UTC): | 13 October 2024 11:36:06 |
| Eccentricity: | 0.0021309 |
| inclination: | 74.0611° |
| perigee height: | 734 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 48.0314° |
| argument of perigee: | 306.9442° |
| revolutions per day: | 14.42685219 |
| mean anomaly at epoch: | 52.9762° |
| orbit number at epoch: | 83228 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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