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 26075.83707009 +.00000000 +00000-0 +42081-4 0 00001
2 20625 70.9974 282.9030 0016153 290.0556 69.8827 14.15011254 04
| Epoch (UTC): | 16 March 2026 20:05:22 |
| Eccentricity: | 0.0016153 |
| inclination: | 70.9974° |
| perigee height: | 831 km |
| apogee height: | 854 km |
| right ascension of ascending node: | 282.9030° |
| argument of perigee: | 290.0556° |
| revolutions per day: | 14.15011254 |
| mean anomaly at epoch: | 69.8827° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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