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 26072.13994532 +.00000000 +00000-0 +27135-3 0 00002
2 20580 28.4723 16.4622 0001799 159.6118 200.4550 15.29543468 04
| Epoch (UTC): | 13 March 2026 03:21:31 |
| Eccentricity: | 0.0001799 |
| inclination: | 28.4723° |
| perigee height: | 476 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 16.4622° |
| argument of perigee: | 159.6118° |
| revolutions per day: | 15.29543468 |
| mean anomaly at epoch: | 200.4550° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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