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 56075U 26145.55986564 +.00000000 +00000-0 +36583-3 0 00000
2 56075 87.8993 263.7382 0001990 110.1719 249.9625 13.15547199 01
| Epoch (UTC): | 25 May 2026 13:26:12 |
| Eccentricity: | 0.0001990 |
| inclination: | 87.8993° |
| perigee height: | 1200 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.7382° |
| argument of perigee: | 110.1719° |
| revolutions per day: | 13.15547199 |
| mean anomaly at epoch: | 249.9625° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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