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 56080U 26145.60740811 +.00000000 +00000-0 +37689-3 0 00003
2 56080 87.8987 263.7204 0002168 99.4462 260.6913 13.15547733 09
| Epoch (UTC): | 25 May 2026 14:34:40 |
| Eccentricity: | 0.0002168 |
| inclination: | 87.8987° |
| perigee height: | 1200 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.7204° |
| argument of perigee: | 99.4462° |
| revolutions per day: | 13.15547733 |
| mean anomaly at epoch: | 260.6913° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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