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 26086.74215743 +.00000000 +00000-0 +52079-3 0 00006
2 39055 98.7430 78.8995 0006845 260.5491 277.5161 14.24369594 07
| Epoch (UTC): | 27 March 2026 17:48:42 |
| Eccentricity: | 0.0006845 |
| inclination: | 98.7430° |
| perigee height: | 806 km |
| apogee height: | 816 km |
| right ascension of ascending node: | 78.8995° |
| argument of perigee: | 260.5491° |
| revolutions per day: | 14.24369594 |
| mean anomaly at epoch: | 277.5161° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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