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 26038.79235705 +.00000000 +00000-0 +26695-3 0 00006
2 20580 28.4662 243.8802 0001811 133.8603 226.2143 15.29001499 07
| Epoch (UTC): | 07 February 2026 19:00:59 |
| Eccentricity: | 0.0001811 |
| inclination: | 28.4662° |
| perigee height: | 478 km |
| apogee height: | 480 km |
| right ascension of ascending node: | 243.8802° |
| argument of perigee: | 133.8603° |
| revolutions per day: | 15.29001499 |
| mean anomaly at epoch: | 226.2143° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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