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 26075.32025727 +.00000000 +00000-0 +18902-3 0 00004
2 27939 98.3443 257.0660 0010841 197.6970 284.4524 14.73274554 03
| Epoch (UTC): | 16 March 2026 07:41:10 |
| Eccentricity: | 0.0010841 |
| inclination: | 98.3443° |
| perigee height: | 643 km |
| apogee height: | 658 km |
| right ascension of ascending node: | 257.0660° |
| argument of perigee: | 197.6970° |
| revolutions per day: | 14.73274554 |
| mean anomaly at epoch: | 284.4524° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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