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 55751U 26145.43519507 +.00000000 +00000-0 +27500-4 0 00006
2 55751 70.0008 51.0459 0002894 269.4267 90.6560 14.98331064 08
| Epoch (UTC): | 25 May 2026 10:26:40 |
| Eccentricity: | 0.0002894 |
| inclination: | 70.0008° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 51.0459° |
| argument of perigee: | 269.4267° |
| revolutions per day: | 14.98331064 |
| mean anomaly at epoch: | 90.6560° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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