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 26068.29830958 +.00000000 +00000-0 +32603-3 0 00009
2 19210 82.5106 158.6408 0012487 123.9186 236.3242 15.28520254 07
| Epoch (UTC): | 09 March 2026 07:09:33 |
| Eccentricity: | 0.0012487 |
| inclination: | 82.5106° |
| perigee height: | 472 km |
| apogee height: | 489 km |
| right ascension of ascending node: | 158.6408° |
| argument of perigee: | 123.9186° |
| revolutions per day: | 15.28520254 |
| mean anomaly at epoch: | 236.3242° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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