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 26074.96963185 +.00000000 +00000-0 +87177-4 0 00006
2 19120 71.0143 55.2672 0023092 325.2120 34.7494 14.19617026 07
| Epoch (UTC): | 15 March 2026 23:16:16 |
| Eccentricity: | 0.0023092 |
| inclination: | 71.0143° |
| perigee height: | 810 km |
| apogee height: | 843 km |
| right ascension of ascending node: | 55.2672° |
| argument of perigee: | 325.2120° |
| revolutions per day: | 14.19617026 |
| mean anomaly at epoch: | 34.7494° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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