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 26107.23666775 +.00000000 +00000-0 +13199-3 0 00002
2 20580 28.4726 136.9211 0002095 181.6672 178.3917 15.30064950 05
| Epoch (UTC): | 17 April 2026 05:40:48 |
| Eccentricity: | 0.0002095 |
| inclination: | 28.4726° |
| perigee height: | 474 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 136.9211° |
| argument of perigee: | 181.6672° |
| revolutions per day: | 15.30064950 |
| mean anomaly at epoch: | 178.3917° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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