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 55629U 26145.58494358 +.00000000 +00000-0 +50316-4 0 00003
2 55629 69.9998 10.6894 0002741 269.5911 90.4934 14.98332121 07
| Epoch (UTC): | 25 May 2026 14:02:19 |
| Eccentricity: | 0.0002741 |
| inclination: | 69.9998° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 10.6894° |
| argument of perigee: | 269.5911° |
| revolutions per day: | 14.98332121 |
| mean anomaly at epoch: | 90.4934° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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