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 26045.51498648 +.00000000 +00000-0 +21547-3 0 00002
2 20580 28.4665 198.0454 0001452 202.8355 157.2176 15.29102662 09
| Epoch (UTC): | 14 February 2026 12:21:34 |
| Eccentricity: | 0.0001452 |
| inclination: | 28.4665° |
| perigee height: | 477 km |
| apogee height: | 479 km |
| right ascension of ascending node: | 198.0454° |
| argument of perigee: | 202.8355° |
| revolutions per day: | 15.29102662 |
| mean anomaly at epoch: | 157.2176° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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