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 23151.96437295 .00003631 00000-0 18924-3 0 9991
2 20580 28.4706 15.9385 0002291 197.3921 191.4430 15.13149238619006
| Epoch (UTC): | 31 May 2023 23:08:41 |
| Eccentricity: | 0.0002291 |
| inclination: | 28.4706° |
| perigee height: | 525 km |
| apogee height: | 528 km |
| right ascension of ascending node: | 15.9385° |
| argument of perigee: | 197.3921° |
| revolutions per day: | 15.13149238 |
| mean anomaly at epoch: | 191.4430° |
| orbit number at epoch: | 61900 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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