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 25134.73891115 .00006617 00000-0 24958-3 0 9995
2 20580 28.4685 271.5829 0002903 78.7476 281.3445 15.24968911727578
| Epoch (UTC): | 14 May 2025 17:44:01 |
| Eccentricity: | 0.0002903 |
| inclination: | 28.4685° |
| perigee height: | 489 km |
| apogee height: | 493 km |
| right ascension of ascending node: | 271.5829° |
| argument of perigee: | 78.7476° |
| revolutions per day: | 15.24968911 |
| mean anomaly at epoch: | 281.3445° |
| orbit number at epoch: | 72757 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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