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 27939U 26109.28693889 +.00000000 +00000-0 +40681-4 0 00007
2 27939 98.3458 291.9861 0012573 94.9573 77.1424 14.73356500 09
| Epoch (UTC): | 19 April 2026 06:53:11 |
| Eccentricity: | 0.0012573 |
| inclination: | 98.3458° |
| perigee height: | 642 km |
| apogee height: | 659 km |
| right ascension of ascending node: | 291.9861° |
| argument of perigee: | 94.9573° |
| revolutions per day: | 14.73356500 |
| mean anomaly at epoch: | 77.1424° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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