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 68592U 26145.10861045 +.00000000 +00000-0 +10951-2 0 00004
2 68592 51.8655 288.9477 0011217 304.7626 55.2304 15.36253379 00
| Epoch (UTC): | 25 May 2026 02:36:23 |
| Eccentricity: | 0.0011217 |
| inclination: | 51.8655° |
| perigee height: | 450 km |
| apogee height: | 465 km |
| right ascension of ascending node: | 288.9477° |
| argument of perigee: | 304.7626° |
| revolutions per day: | 15.36253379 |
| mean anomaly at epoch: | 55.2304° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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