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 25197.22437354 .00003263 00000-0 11677-3 0 9997
2 20580 28.4669 208.0543 0002181 61.0879 298.9934 15.25566610737386
| Epoch (UTC): | 16 July 2025 05:23:05 |
| Eccentricity: | 0.0002181 |
| inclination: | 28.4669° |
| perigee height: | 487 km |
| apogee height: | 490 km |
| right ascension of ascending node: | 208.0543° |
| argument of perigee: | 61.0879° |
| revolutions per day: | 15.25566610 |
| mean anomaly at epoch: | 298.9934° |
| orbit number at epoch: | 73738 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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