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 25137.61839470 .00008126 00000-0 30797-3 0 9996
2 20580 28.4681 252.0748 0002898 106.8448 253.2464 15.25008337728010
| Epoch (UTC): | 17 May 2025 14:50:29 |
| Eccentricity: | 0.0002898 |
| inclination: | 28.4681° |
| perigee height: | 489 km |
| apogee height: | 493 km |
| right ascension of ascending node: | 252.0748° |
| argument of perigee: | 106.8448° |
| revolutions per day: | 15.25008337 |
| mean anomaly at epoch: | 253.2464° |
| orbit number at epoch: | 72801 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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