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 55914U 26145.33158047 +.00000000 +00000-0 +93298-5 0 00002
2 55914 69.9992 111.3691 0003399 268.4668 91.6102 14.98331862 00
| Epoch (UTC): | 25 May 2026 07:57:28 |
| Eccentricity: | 0.0003399 |
| inclination: | 69.9992° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 111.3691° |
| argument of perigee: | 268.4668° |
| revolutions per day: | 14.98331862 |
| mean anomaly at epoch: | 91.6102° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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