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 28654U 26066.41854824 +.00000000 +00000-0 +67483-4 0 00006
2 28654 98.8159 147.5576 0015314 81.4857 278.8050 14.13710289 05
| Epoch (UTC): | 07 March 2026 10:02:42 |
| Eccentricity: | 0.0015314 |
| inclination: | 98.8159° |
| perigee height: | 836 km |
| apogee height: | 858 km |
| right ascension of ascending node: | 147.5576° |
| argument of perigee: | 81.4857° |
| revolutions per day: | 14.13710289 |
| mean anomaly at epoch: | 278.8050° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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