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 56098U 26145.18769051 +.00000000 +00000-0 +80825-5 0 00004
2 56098 43.0050 89.3054 0001437 264.1162 95.9526 15.27574651 07
| Epoch (UTC): | 25 May 2026 04:30:16 |
| Eccentricity: | 0.0001437 |
| inclination: | 43.0050° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 89.3054° |
| argument of perigee: | 264.1162° |
| revolutions per day: | 15.27574651 |
| mean anomaly at epoch: | 95.9526° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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