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 26153.99330192 +.00000000 +00000-0 +62173-3 0 00000
2 20712 18.1217 306.4151 7076076 275.2485 14.6646 2.50063047 04
| Epoch (UTC): | 02 June 2026 23:50:21 |
| Eccentricity: | 0.7076076 |
| inclination: | 18.1217° |
| perigee height: | 326 km |
| apogee height: | 32774 km |
| right ascension of ascending node: | 306.4151° |
| argument of perigee: | 275.2485° |
| revolutions per day: | 2.50063047 |
| mean anomaly at epoch: | 14.6646° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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