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 19211U 26042.20248632 +.00000000 +00000-0 +58202-4 0 00009
2 19211 82.5268 123.2835 0022108 129.9498 230.3665 14.85356645 08
| Epoch (UTC): | 11 February 2026 04:51:34 |
| Eccentricity: | 0.0022108 |
| inclination: | 82.5268° |
| perigee height: | 597 km |
| apogee height: | 628 km |
| right ascension of ascending node: | 123.2835° |
| argument of perigee: | 129.9498° |
| revolutions per day: | 14.85356645 |
| mean anomaly at epoch: | 230.3665° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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