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 26128.21958413 +.00000000 +00000-0 +10779-3 0 00007
2 20625 70.9985 172.8884 0015600 220.9191 139.0762 14.15022436 05
| Epoch (UTC): | 08 May 2026 05:16:12 |
| Eccentricity: | 0.0015600 |
| inclination: | 70.9985° |
| perigee height: | 831 km |
| apogee height: | 854 km |
| right ascension of ascending node: | 172.8884° |
| argument of perigee: | 220.9191° |
| revolutions per day: | 14.15022436 |
| mean anomaly at epoch: | 139.0762° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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