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 26064.76311507 +.00000000 +00000-0 +39909-3 0 00007
2 19210 82.5107 162.1946 0012321 134.9628 225.2613 15.28442727 02
| Epoch (UTC): | 05 March 2026 18:18:53 |
| Eccentricity: | 0.0012321 |
| inclination: | 82.5107° |
| perigee height: | 472 km |
| apogee height: | 489 km |
| right ascension of ascending node: | 162.1946° |
| argument of perigee: | 134.9628° |
| revolutions per day: | 15.28442727 |
| mean anomaly at epoch: | 225.2613° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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