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 26053.73549034 +.00000000 +00000-0 +55978-4 0 00008
2 15055 82.9612 162.7459 0027349 13.3725 95.7672 13.74548196 00
| Epoch (UTC): | 22 February 2026 17:39:06 |
| Eccentricity: | 0.0027349 |
| inclination: | 82.9612° |
| perigee height: | 963 km |
| apogee height: | 1003 km |
| right ascension of ascending node: | 162.7459° |
| argument of perigee: | 13.3725° |
| revolutions per day: | 13.74548196 |
| mean anomaly at epoch: | 95.7672° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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