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 26106.97425943 +.00000000 +00000-0 +16452-3 0 00002
2 27939 98.3459 289.6087 0012531 101.5368 51.2611 14.73356919 00
| Epoch (UTC): | 16 April 2026 23:22:56 |
| Eccentricity: | 0.0012531 |
| inclination: | 98.3459° |
| perigee height: | 642 km |
| apogee height: | 659 km |
| right ascension of ascending node: | 289.6087° |
| argument of perigee: | 101.5368° |
| revolutions per day: | 14.73356919 |
| mean anomaly at epoch: | 51.2611° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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