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 20401U 26104.00988866 +.00000000 +00000-0 +00000-0 0 00008
2 20401 12.5223 350.0078 0015221 316.0754 227.9808 0.99000586 07
| Epoch (UTC): | 14 April 2026 00:14:14 |
| Eccentricity: | 0.0015221 |
| inclination: | 12.5223° |
| perigee height: | 36082 km |
| apogee height: | 36212 km |
| right ascension of ascending node: | 350.0078° |
| argument of perigee: | 316.0754° |
| revolutions per day: | 0.99000586 |
| mean anomaly at epoch: | 227.9808° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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