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 55952U 26145.21862139 +.00000000 +00000-0 +20032-4 0 00000
2 55952 70.0002 71.6160 0003094 269.2242 90.8562 14.98333013 06
| Epoch (UTC): | 25 May 2026 05:14:48 |
| Eccentricity: | 0.0003094 |
| inclination: | 70.0002° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 71.6160° |
| argument of perigee: | 269.2242° |
| revolutions per day: | 14.98333013 |
| mean anomaly at epoch: | 90.8562° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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