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 68753U 26145.61615649 +.00000000 +00000-0 +15689-3 0 00000
2 68753 98.2701 294.7179 0062468 307.1035 52.4499 15.22285291 02
| Epoch (UTC): | 25 May 2026 14:47:15 |
| Eccentricity: | 0.0062468 |
| inclination: | 98.2701° |
| perigee height: | 456 km |
| apogee height: | 542 km |
| right ascension of ascending node: | 294.7179° |
| argument of perigee: | 307.1035° |
| revolutions per day: | 15.22285291 |
| mean anomaly at epoch: | 52.4499° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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