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 21112.76785590 .00000106 00000-0 45260-4 0 9996
2 00085 38.7746 241.6661 0387559 41.7128 321.2500 14.21639156975110
| Epoch (UTC): | 22 April 2021 18:25:42 |
| Eccentricity: | 0.0387559 |
| inclination: | 38.7746° |
| perigee height: | 541 km |
| apogee height: | 1099 km |
| right ascension of ascending node: | 241.6661° |
| argument of perigee: | 41.7128° |
| revolutions per day: | 14.21639156 |
| mean anomaly at epoch: | 321.2500° |
| orbit number at epoch: | 97511 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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