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 15055U 26104.09649696 +.00000000 +00000-0 +57902-4 0 00008
2 15055 82.9541 125.5550 0026154 227.9385 186.3211 13.74553762 09
| Epoch (UTC): | 14 April 2026 02:18:57 |
| Eccentricity: | 0.0026154 |
| inclination: | 82.9541° |
| perigee height: | 964 km |
| apogee height: | 1003 km |
| right ascension of ascending node: | 125.5550° |
| argument of perigee: | 227.9385° |
| revolutions per day: | 13.74553762 |
| mean anomaly at epoch: | 186.3211° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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