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 26037.81329490 +.00000000 +00000-0 +28897-3 0 00009
2 20580 28.4665 250.5538 0001883 124.2340 235.8434 15.28986369 08
| Epoch (UTC): | 06 February 2026 19:31:08 |
| Eccentricity: | 0.0001883 |
| inclination: | 28.4665° |
| perigee height: | 478 km |
| apogee height: | 480 km |
| right ascension of ascending node: | 250.5538° |
| argument of perigee: | 124.2340° |
| revolutions per day: | 15.28986369 |
| mean anomaly at epoch: | 235.8434° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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