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 37753U 26145.42926007 +.00000000 +00000-0 +00000-0 0 00006
2 37753 56.5755 332.9045 0142030 62.2143 297.5817 2.00562561 00
| Epoch (UTC): | 25 May 2026 10:18:08 |
| Eccentricity: | 0.0142030 |
| inclination: | 56.5755° |
| perigee height: | 19805 km |
| apogee height: | 20560 km |
| right ascension of ascending node: | 332.9045° |
| argument of perigee: | 62.2143° |
| revolutions per day: | 2.00562561 |
| mean anomaly at epoch: | 297.5817° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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