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 12719U 26108.21409227 +.00000000 +00000-0 +27330-3 0 00005
2 12719 82.9571 86.1362 0022071 157.9040 223.6636 13.94520293 04
| Epoch (UTC): | 18 April 2026 05:08:17 |
| Eccentricity: | 0.0022071 |
| inclination: | 82.9571° |
| perigee height: | 897 km |
| apogee height: | 929 km |
| right ascension of ascending node: | 86.1362° |
| argument of perigee: | 157.9040° |
| revolutions per day: | 13.94520293 |
| mean anomaly at epoch: | 223.6636° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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