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 25162.87683047 .00004542 00000-0 16727-3 0 9994
2 20580 28.4685 80.9077 0002578 36.3649 323.7121 15.25263214731870
| Epoch (UTC): | 11 June 2025 21:02:38 |
| Eccentricity: | 0.0002578 |
| inclination: | 28.4685° |
| perigee height: | 488 km |
| apogee height: | 492 km |
| right ascension of ascending node: | 80.9077° |
| argument of perigee: | 36.3649° |
| revolutions per day: | 15.25263214 |
| mean anomaly at epoch: | 323.7121° |
| orbit number at epoch: | 73187 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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