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 23029.91954961 .00003760 00000-0 20410-3 0 9990
2 20580 28.4702 107.0657 0002088 332.3183 192.1732 15.11792117600777
| Epoch (UTC): | 29 January 2023 22:04:09 |
| Eccentricity: | 0.0002088 |
| inclination: | 28.4702° |
| perigee height: | 529 km |
| apogee height: | 532 km |
| right ascension of ascending node: | 107.0657° |
| argument of perigee: | 332.3183° |
| revolutions per day: | 15.11792117 |
| mean anomaly at epoch: | 192.1732° |
| orbit number at epoch: | 60077 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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