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 28096U 26017.29347617 +.00000000 +00000-0 +56724-4 0 00001
2 28096 63.6803 56.0743 0075501 123.4210 237.4067 13.41057727 05
| Epoch (UTC): | 17 January 2026 07:02:36 |
| Eccentricity: | 0.0075501 |
| inclination: | 63.6803° |
| perigee height: | 1049 km |
| apogee height: | 1162 km |
| right ascension of ascending node: | 56.0743° |
| argument of perigee: | 123.4210° |
| revolutions per day: | 13.41057727 |
| mean anomaly at epoch: | 237.4067° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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