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 28493U 26145.31955333 +.00000000 +00000-0 +12640-3 0 00005
2 28493 98.2245 281.4263 0004288 24.8121 335.3295 14.80105619 09
| Epoch (UTC): | 25 May 2026 07:40:09 |
| Eccentricity: | 0.0004288 |
| inclination: | 98.2245° |
| perigee height: | 626 km |
| apogee height: | 632 km |
| right ascension of ascending node: | 281.4263° |
| argument of perigee: | 24.8121° |
| revolutions per day: | 14.80105619 |
| mean anomaly at epoch: | 335.3295° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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