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 27704U 26140.56982993 +.00000000 +00000-0 +00000-0 0 00007
2 27704 54.8300 326.1803 0003007 1.9314 320.9052 1.94743016 09
| Epoch (UTC): | 20 May 2026 13:40:33 |
| Eccentricity: | 0.0003007 |
| inclination: | 54.8300° |
| perigee height: | 20701 km |
| apogee height: | 20717 km |
| right ascension of ascending node: | 326.1803° |
| argument of perigee: | 1.9314° |
| revolutions per day: | 1.94743016 |
| mean anomaly at epoch: | 320.9052° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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