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 19210U 26158.86199764 +.00000000 +00000-0 +25990-3 0 00006
2 19210 82.5076 67.4365 0011326 155.4063 204.7720 15.29847324 08
| Epoch (UTC): | 07 June 2026 20:41:16 |
| Eccentricity: | 0.0011326 |
| inclination: | 82.5076° |
| perigee height: | 469 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 67.4365° |
| argument of perigee: | 155.4063° |
| revolutions per day: | 15.29847324 |
| mean anomaly at epoch: | 204.7720° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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