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 37180U 26150.47051131 +.00000000 +00000-0 +12129-3 0 00006
2 37180 97.8680 155.7014 0010273 9.0911 351.0496 14.99275011 02
| Epoch (UTC): | 30 May 2026 11:17:32 |
| Eccentricity: | 0.0010273 |
| inclination: | 97.8680° |
| perigee height: | 562 km |
| apogee height: | 576 km |
| right ascension of ascending node: | 155.7014° |
| argument of perigee: | 9.0911° |
| revolutions per day: | 14.99275011 |
| mean anomaly at epoch: | 351.0496° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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