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 20580U 90037B 22144.84358394 .00003429 00000-0 19211-3 0 9996
2 20580 28.4703 325.2376 0002762 135.1306 322.7952 15.10499948562648
| Epoch (UTC): | 24 May 2022 20:14:45 |
| Eccentricity: | 0.0002762 |
| inclination: | 28.4703° |
| perigee height: | 533 km |
| apogee height: | 536 km |
| right ascension of ascending node: | 325.2376° |
| argument of perigee: | 135.1306° |
| revolutions per day: | 15.10499948 |
| mean anomaly at epoch: | 322.7952° |
| orbit number at epoch: | 56264 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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