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 28485U 04047A 18294.37688272 .00000872 00000-0 29580-4 0 9994
2 28485 20.5574 299.4408 0011021 326.5722 33.4016 15.04220886762255
| Epoch (UTC): | 21 October 2018 09:02:42 |
| Eccentricity: | 0.0011021 |
| inclination: | 20.5574° |
| perigee height: | 546 km |
| apogee height: | 561 km |
| right ascension of ascending node: | 299.4408° |
| argument of perigee: | 326.5722° |
| revolutions per day: | 15.04220886 |
| mean anomaly at epoch: | 33.4016° |
| orbit number at epoch: | 76225 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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