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 19119U 26076.20665499 +.00000000 +00000-0 +19043-3 0 00006
2 19119 71.0020 230.1192 0013304 241.1617 291.6023 14.15743218 03
| Epoch (UTC): | 17 March 2026 04:57:34 |
| Eccentricity: | 0.0013304 |
| inclination: | 71.0020° |
| perigee height: | 830 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 230.1192° |
| argument of perigee: | 241.1617° |
| revolutions per day: | 14.15743218 |
| mean anomaly at epoch: | 291.6023° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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