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 39127U 26145.56249500 +.00000000 +00000-0 +00000-0 0 00004
2 39127 0.0167 345.7037 0001896 73.1769 279.4467 1.00271785 04
| Epoch (UTC): | 25 May 2026 13:29:59 |
| Eccentricity: | 0.0001896 |
| inclination: | 0.0167° |
| perigee height: | 35779 km |
| apogee height: | 35795 km |
| right ascension of ascending node: | 345.7037° |
| argument of perigee: | 73.1769° |
| revolutions per day: | 1.00271785 |
| mean anomaly at epoch: | 279.4467° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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