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 25169.02718269 .00005169 00000-0 19105-3 0 9992
2 20580 28.4692 39.2207 0002605 98.8968 261.1922 15.25335009733078
| Epoch (UTC): | 18 June 2025 00:39:08 |
| Eccentricity: | 0.0002605 |
| inclination: | 28.4692° |
| perigee height: | 488 km |
| apogee height: | 491 km |
| right ascension of ascending node: | 39.2207° |
| argument of perigee: | 98.8968° |
| revolutions per day: | 15.25335009 |
| mean anomaly at epoch: | 261.1922° |
| orbit number at epoch: | 73307 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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