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 20509U 26088.13573735 +.00000000 +00000-0 +16307-3 0 00007
2 20509 82.9493 110.3576 0042333 202.4772 157.4532 13.75880980 01
| Epoch (UTC): | 29 March 2026 03:15:27 |
| Eccentricity: | 0.0042333 |
| inclination: | 82.9493° |
| perigee height: | 947 km |
| apogee height: | 1010 km |
| right ascension of ascending node: | 110.3576° |
| argument of perigee: | 202.4772° |
| revolutions per day: | 13.75880980 |
| mean anomaly at epoch: | 157.4532° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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