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 26150.32219215 +.00000000 +00000-0 +18819-3 0 00008
2 28493 98.2251 286.5493 0003940 9.9003 350.2285 14.80119604 08
| Epoch (UTC): | 30 May 2026 07:43:57 |
| Eccentricity: | 0.0003940 |
| inclination: | 98.2251° |
| perigee height: | 626 km |
| apogee height: | 632 km |
| right ascension of ascending node: | 286.5493° |
| argument of perigee: | 9.9003° |
| revolutions per day: | 14.80119604 |
| mean anomaly at epoch: | 350.2285° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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