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 26074.25539619 +.00000000 +00000-0 +30056-3 0 00002
2 19210 82.5102 152.6499 0012608 104.9751 255.2886 15.28628430 08
| Epoch (UTC): | 15 March 2026 06:07:46 |
| Eccentricity: | 0.0012608 |
| inclination: | 82.5102° |
| perigee height: | 471 km |
| apogee height: | 489 km |
| right ascension of ascending node: | 152.6499° |
| argument of perigee: | 104.9751° |
| revolutions per day: | 15.28628430 |
| mean anomaly at epoch: | 255.2886° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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