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 26142.21852351 +.00000000 +00000-0 +45144-4 0 00002
2 28654 98.8112 222.2715 0013544 221.3904 138.6243 14.13723974 03
| Epoch (UTC): | 22 May 2026 05:14:40 |
| Eccentricity: | 0.0013544 |
| inclination: | 98.8112° |
| perigee height: | 837 km |
| apogee height: | 856 km |
| right ascension of ascending node: | 222.2715° |
| argument of perigee: | 221.3904° |
| revolutions per day: | 14.13723974 |
| mean anomaly at epoch: | 138.6243° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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