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 37932U 26157.14484691 +.00000000 +00000-0 +78748-4 0 00003
2 37932 98.8892 112.5481 0035576 291.7003 78.9125 14.23021955 04
| Epoch (UTC): | 06 June 2026 03:28:34 |
| Eccentricity: | 0.0035576 |
| inclination: | 98.8892° |
| perigee height: | 790 km |
| apogee height: | 841 km |
| right ascension of ascending node: | 112.5481° |
| argument of perigee: | 291.7003° |
| revolutions per day: | 14.23021955 |
| mean anomaly at epoch: | 78.9125° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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