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 00085U 61004C 23339.36394587 .00021359 00000-0 32622-2 0 9996
2 00085 38.7502 333.7393 0289068 27.7257 333.8584 14.48905166112039
| Epoch (UTC): | 05 December 2023 08:44:04 |
| Eccentricity: | 0.0289068 |
| inclination: | 38.7502° |
| perigee height: | 524 km |
| apogee height: | 934 km |
| right ascension of ascending node: | 333.7393° |
| argument of perigee: | 27.7257° |
| revolutions per day: | 14.48905166 |
| mean anomaly at epoch: | 333.8584° |
| orbit number at epoch: | 11203 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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