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 27039U 26109.96731699 +.00000000 +00000-0 +68018-3 0 00008
2 27039 7.7124 180.2987 7169012 233.1544 92.3746 2.26234588 08
| Epoch (UTC): | 19 April 2026 23:12:56 |
| Eccentricity: | 0.7169012 |
| inclination: | 7.7124° |
| perigee height: | 561 km |
| apogee height: | 35705 km |
| right ascension of ascending node: | 180.2987° |
| argument of perigee: | 233.1544° |
| revolutions per day: | 2.26234588 |
| mean anomaly at epoch: | 92.3746° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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