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 is defined by the following mean orbital elements,
1 20580U 26039.77140969 +.00000000 +00000-0 +24335-3 0 00001
2 20580 28.4663 237.2056 0001773 143.0565 217.0153 15.29015568 04
| Epoch (UTC): | 08 February 2026 18:30:49 |
| Eccentricity: | 0.0001773 |
| inclination: | 28.4663° |
| perigee height: | 478 km |
| apogee height: | 480 km |
| right ascension of ascending node: | 237.2056° |
| argument of perigee: | 143.0565° |
| revolutions per day: | 15.29015568 |
| mean anomaly at epoch: | 217.0153° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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