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 56076U 26145.55512654 +.00000000 +00000-0 +51233-3 0 00005
2 56076 87.9002 263.6998 0002125 95.3430 264.7943 13.15549328 05
| Epoch (UTC): | 25 May 2026 13:19:22 |
| Eccentricity: | 0.0002125 |
| inclination: | 87.9002° |
| perigee height: | 1200 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.6998° |
| argument of perigee: | 95.3430° |
| revolutions per day: | 13.15549328 |
| mean anomaly at epoch: | 264.7943° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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