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 41584U 16036A 21250.72513855 0.00000000 00000-0 00000-0 0 07
2 41584 6.3093 353.0682 0049199 54.7537 305.7280 1.00270000 00
| Epoch (UTC): | 07 September 2021 17:24:11 |
| Eccentricity: | 0.0049199 |
| inclination: | 6.3093° |
| perigee height: | 35579 km |
| apogee height: | 35994 km |
| right ascension of ascending node: | 353.0682° |
| argument of perigee: | 54.7537° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 305.7280° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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