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 20625U 26129.63341125 +.00000000 +00000-0 +77090-4 0 00000
2 20625 70.9983 169.9191 0015548 219.1498 140.8501 14.15022961 06
| Epoch (UTC): | 09 May 2026 15:12:06 |
| Eccentricity: | 0.0015548 |
| inclination: | 70.9983° |
| perigee height: | 831 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 169.9191° |
| argument of perigee: | 219.1498° |
| revolutions per day: | 14.15022961 |
| mean anomaly at epoch: | 140.8501° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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