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 67782U 26145.58191222 +.00000000 +00000-0 +17909-2 0 00009
2 67782 51.8984 220.7465 0000247 278.7654 81.3280 14.79915767 03
| Epoch (UTC): | 25 May 2026 13:57:57 |
| Eccentricity: | 0.0000247 |
| inclination: | 51.8984° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 220.7465° |
| argument of perigee: | 278.7654° |
| revolutions per day: | 14.79915767 |
| mean anomaly at epoch: | 81.3280° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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