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 67778U 26144.93763470 +.00000000 +00000-0 +37241-3 0 00004
2 67778 51.8987 226.0238 0000390 113.1723 246.9280 14.79948335 02
| Epoch (UTC): | 24 May 2026 22:30:11 |
| Eccentricity: | 0.0000390 |
| inclination: | 51.8987° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 226.0238° |
| argument of perigee: | 113.1723° |
| revolutions per day: | 14.79948335 |
| mean anomaly at epoch: | 246.9280° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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