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 20624U 90046A 21015.67685013 .00000128 00000-0 91651-4 0 9995
2 20624 71.0417 355.6100 0015652 200.3425 159.7076 14.14353594582190
| Epoch (UTC): | 15 January 2021 16:14:39 |
| Eccentricity: | 0.0015652 |
| inclination: | 71.0417° |
| perigee height: | 833 km |
| apogee height: | 856 km |
| right ascension of ascending node: | 355.6100° |
| argument of perigee: | 200.3425° |
| revolutions per day: | 14.14353594 |
| mean anomaly at epoch: | 159.7076° |
| orbit number at epoch: | 58219 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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