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 55949U 26145.49384626 +.00000000 +00000-0 +88568-5 0 00005
2 55949 70.0004 70.9717 0002932 269.1730 90.9093 14.98330809 05
| Epoch (UTC): | 25 May 2026 11:51:08 |
| Eccentricity: | 0.0002932 |
| inclination: | 70.0004° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 70.9717° |
| argument of perigee: | 269.1730° |
| revolutions per day: | 14.98330809 |
| mean anomaly at epoch: | 90.9093° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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