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 69178U 26142.82108852 +.00000000 +00000-0 +30623-4 0 00001
2 69178 44.9111 325.6435 0027869 269.2056 90.5623 15.02347412 07
| Epoch (UTC): | 22 May 2026 19:42:22 |
| Eccentricity: | 0.0027869 |
| inclination: | 44.9111° |
| perigee height: | 540 km |
| apogee height: | 579 km |
| right ascension of ascending node: | 325.6435° |
| argument of perigee: | 269.2056° |
| revolutions per day: | 15.02347412 |
| mean anomaly at epoch: | 90.5623° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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