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 26106.81384656 +.00000000 +00000-0 +41239-4 0 00008
2 15055 82.9539 123.5471 0026285 220.0923 313.1063 13.74553941 07
| Epoch (UTC): | 16 April 2026 19:31:56 |
| Eccentricity: | 0.0026285 |
| inclination: | 82.9539° |
| perigee height: | 964 km |
| apogee height: | 1003 km |
| right ascension of ascending node: | 123.5471° |
| argument of perigee: | 220.0923° |
| revolutions per day: | 13.74553941 |
| mean anomaly at epoch: | 313.1063° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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