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 26107.61917882 +.00000000 +00000-0 +61653-3 0 00007
2 20712 18.1485 326.4217 7080329 237.9989 34.3548 2.49982299 03
| Epoch (UTC): | 17 April 2026 14:51:37 |
| Eccentricity: | 0.7080329 |
| inclination: | 18.1485° |
| perigee height: | 318 km |
| apogee height: | 32792 km |
| right ascension of ascending node: | 326.4217° |
| argument of perigee: | 237.9989° |
| revolutions per day: | 2.49982299 |
| mean anomaly at epoch: | 34.3548° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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