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 26101.33171389 +.00000000 +00000-0 +10209-3 0 00003
2 27939 98.3468 283.8066 0012360 117.6025 4.6448 14.73347149 06
| Epoch (UTC): | 11 April 2026 07:57:40 |
| Eccentricity: | 0.0012360 |
| inclination: | 98.3468° |
| perigee height: | 642 km |
| apogee height: | 659 km |
| right ascension of ascending node: | 283.8066° |
| argument of perigee: | 117.6025° |
| revolutions per day: | 14.73347149 |
| mean anomaly at epoch: | 4.6448° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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