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 19531U 26159.45579448 +.00000000 +00000-0 +50361-4 0 00000
2 19531 98.6194 105.5063 0010467 328.8342 31.2210 14.15837761 08
| Epoch (UTC): | 08 June 2026 10:56:20 |
| Eccentricity: | 0.0010467 |
| inclination: | 98.6194° |
| perigee height: | 832 km |
| apogee height: | 847 km |
| right ascension of ascending node: | 105.5063° |
| argument of perigee: | 328.8342° |
| revolutions per day: | 14.15837761 |
| mean anomaly at epoch: | 31.2210° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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