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 26036.89949413 +.00000000 +00000-0 +32208-3 0 00000
2 20580 28.4665 256.7833 0001911 115.5134 244.5659 15.28971962 09
| Epoch (UTC): | 05 February 2026 21:35:16 |
| Eccentricity: | 0.0001911 |
| inclination: | 28.4665° |
| perigee height: | 478 km |
| apogee height: | 480 km |
| right ascension of ascending node: | 256.7833° |
| argument of perigee: | 115.5134° |
| revolutions per day: | 15.28971962 |
| mean anomaly at epoch: | 244.5659° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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