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 26042.31189992 +.00000000 +00000-0 +19376-3 0 00008
2 27939 98.3410 223.1435 0010522 312.4009 171.1921 14.73175784 05
| Epoch (UTC): | 11 February 2026 07:29:08 |
| Eccentricity: | 0.0010522 |
| inclination: | 98.3410° |
| perigee height: | 644 km |
| apogee height: | 658 km |
| right ascension of ascending node: | 223.1435° |
| argument of perigee: | 312.4009° |
| revolutions per day: | 14.73175784 |
| mean anomaly at epoch: | 171.1921° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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