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 19120U 26074.33546862 +.00000000 +00000-0 +10043-3 0 00003
2 19120 71.0142 56.6082 0023061 326.1268 33.8383 14.19616804 05
| Epoch (UTC): | 15 March 2026 08:03:04 |
| Eccentricity: | 0.0023061 |
| inclination: | 71.0142° |
| perigee height: | 810 km |
| apogee height: | 843 km |
| right ascension of ascending node: | 56.6082° |
| argument of perigee: | 326.1268° |
| revolutions per day: | 14.19616804 |
| mean anomaly at epoch: | 33.8383° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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