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 39055U 26091.72902059 +.00000000 +00000-0 +65910-3 0 00001
2 39055 98.7451 83.8637 0005667 240.2159 294.8294 14.24385845 02
| Epoch (UTC): | 01 April 2026 17:29:47 |
| Eccentricity: | 0.0005667 |
| inclination: | 98.7451° |
| perigee height: | 806 km |
| apogee height: | 815 km |
| right ascension of ascending node: | 83.8637° |
| argument of perigee: | 240.2159° |
| revolutions per day: | 14.24385845 |
| mean anomaly at epoch: | 294.8294° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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