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 21056.31957478 .00001334 00000-0 60636-4 0 9996
2 28485 20.5576 54.3962 0011077 17.6047 342.4769 15.04874469891588
| Epoch (UTC): | 25 February 2021 07:40:11 |
| Eccentricity: | 0.0011077 |
| inclination: | 20.5576° |
| perigee height: | 544 km |
| apogee height: | 559 km |
| right ascension of ascending node: | 54.3962° |
| argument of perigee: | 17.6047° |
| revolutions per day: | 15.04874469 |
| mean anomaly at epoch: | 342.4769° |
| orbit number at epoch: | 89158 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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