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 56719U 26145.31427458 +.00000000 +00000-0 +47403-3 0 00004
2 56719 87.9000 263.7495 0001979 108.3423 251.7923 13.15547349 08
| Epoch (UTC): | 25 May 2026 07:32:33 |
| Eccentricity: | 0.0001979 |
| inclination: | 87.9000° |
| perigee height: | 1200 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.7495° |
| argument of perigee: | 108.3423° |
| revolutions per day: | 13.15547349 |
| mean anomaly at epoch: | 251.7923° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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