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 27941U 26150.42168654 +.00000000 +00000-0 +15897-3 0 00009
2 27941 98.0041 341.9635 0042024 350.1248 9.9139 14.90269933 00
| Epoch (UTC): | 30 May 2026 10:07:13 |
| Eccentricity: | 0.0042024 |
| inclination: | 98.0041° |
| perigee height: | 568 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 341.9635° |
| argument of perigee: | 350.1248° |
| revolutions per day: | 14.90269933 |
| mean anomaly at epoch: | 9.9139° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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