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 40028U 14033U 21023.80990003 .00000127 00000-0 19468-4 0 9994
2 40028 97.9332 315.0495 0012438 297.5140 62.4819 14.89123326358366
| Epoch (UTC): | 23 January 2021 19:26:15 |
| Eccentricity: | 0.0012438 |
| inclination: | 97.9332° |
| perigee height: | 592 km |
| apogee height: | 609 km |
| right ascension of ascending node: | 315.0495° |
| argument of perigee: | 297.5140° |
| revolutions per day: | 14.89123326 |
| mean anomaly at epoch: | 62.4819° |
| orbit number at epoch: | 35836 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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