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 37167U 26145.60769924 +.00000000 +00000-0 +12525-3 0 00006
2 37167 97.9764 126.9793 0019368 6.3531 353.7928 14.90857492 06
| Epoch (UTC): | 25 May 2026 14:35:05 |
| Eccentricity: | 0.0019368 |
| inclination: | 97.9764° |
| perigee height: | 582 km |
| apogee height: | 609 km |
| right ascension of ascending node: | 126.9793° |
| argument of perigee: | 6.3531° |
| revolutions per day: | 14.90857492 |
| mean anomaly at epoch: | 353.7928° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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