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 26160.06551713 +.00000000 +00000-0 +45166-4 0 00008
2 15055 82.9574 84.2032 0028696 74.5126 300.8870 13.74558752 01
| Epoch (UTC): | 09 June 2026 01:34:20 |
| Eccentricity: | 0.0028696 |
| inclination: | 82.9574° |
| perigee height: | 962 km |
| apogee height: | 1004 km |
| right ascension of ascending node: | 84.2032° |
| argument of perigee: | 74.5126° |
| revolutions per day: | 13.74558752 |
| mean anomaly at epoch: | 300.8870° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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