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 56718U 26145.36655876 +.00000000 +00000-0 -44074-4 0 00008
2 56718 87.8995 263.7398 0002293 111.5010 248.6365 13.15547477 06
| Epoch (UTC): | 25 May 2026 08:47:50 |
| Eccentricity: | 0.0002293 |
| inclination: | 87.8995° |
| perigee height: | 1200 km |
| apogee height: | 1204 km |
| right ascension of ascending node: | 263.7398° |
| argument of perigee: | 111.5010° |
| revolutions per day: | 13.15547477 |
| mean anomaly at epoch: | 248.6365° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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