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 20712U 26062.87992142 +.00000000 +00000-0 +10603-2 0 00005
2 20712 18.1578 345.8124 7078392 201.9817 98.4933 2.49897588 01
| Epoch (UTC): | 03 March 2026 21:07:05 |
| Eccentricity: | 0.7078392 |
| inclination: | 18.1578° |
| perigee height: | 324 km |
| apogee height: | 32797 km |
| right ascension of ascending node: | 345.8124° |
| argument of perigee: | 201.9817° |
| revolutions per day: | 2.49897588 |
| mean anomaly at epoch: | 98.4933° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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