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 37791U 26150.87750933 +.00000000 +00000-0 +14864-3 0 00002
2 37791 98.0571 242.5387 0019265 245.9559 233.7856 14.68148549 06
| Epoch (UTC): | 30 May 2026 21:03:36 |
| Eccentricity: | 0.0019265 |
| inclination: | 98.0571° |
| perigee height: | 653 km |
| apogee height: | 681 km |
| right ascension of ascending node: | 242.5387° |
| argument of perigee: | 245.9559° |
| revolutions per day: | 14.68148549 |
| mean anomaly at epoch: | 233.7856° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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