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 55956U 26145.24764795 +.00000000 +00000-0 +14960-4 0 00009
2 55956 70.0007 71.3164 0002888 269.9132 90.1696 14.98332817 03
| Epoch (UTC): | 25 May 2026 05:56:36 |
| Eccentricity: | 0.0002888 |
| inclination: | 70.0007° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 71.3164° |
| argument of perigee: | 269.9132° |
| revolutions per day: | 14.98332817 |
| mean anomaly at epoch: | 90.1696° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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