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 23271.54555714 .00043391 00000-0 70693-2 0 9992
2 00085 38.7537 333.9454 0307341 276.1556 80.4269 14.43488785102216
| Epoch (UTC): | 28 September 2023 13:05:36 |
| Eccentricity: | 0.0307341 |
| inclination: | 38.7537° |
| perigee height: | 528 km |
| apogee height: | 966 km |
| right ascension of ascending node: | 333.9454° |
| argument of perigee: | 276.1556° |
| revolutions per day: | 14.43488785 |
| mean anomaly at epoch: | 80.4269° |
| orbit number at epoch: | 10221 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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