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 26155.32129924 +.00000000 +00000-0 +17509-3 0 00009
2 27939 98.3465 339.3166 0010398 315.2695 168.2196 14.73443963 07
| Epoch (UTC): | 04 June 2026 07:42:40 |
| Eccentricity: | 0.0010398 |
| inclination: | 98.3465° |
| perigee height: | 643 km |
| apogee height: | 657 km |
| right ascension of ascending node: | 339.3166° |
| argument of perigee: | 315.2695° |
| revolutions per day: | 14.73443963 |
| mean anomaly at epoch: | 168.2196° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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