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 20705U 26150.22365800 +.00000000 +00000-0 +00000-0 0 00007
2 20705 15.2000 358.5088 0045738 330.4022 27.9868 0.98609263 05
| Epoch (UTC): | 30 May 2026 05:22:04 |
| Eccentricity: | 0.0045738 |
| inclination: | 15.2000° |
| perigee height: | 36064 km |
| apogee height: | 36454 km |
| right ascension of ascending node: | 358.5088° |
| argument of perigee: | 330.4022° |
| revolutions per day: | 0.98609263 |
| mean anomaly at epoch: | 27.9868° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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