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 55959U 26145.53139278 +.00000000 +00000-0 +10132-3 0 00002
2 55959 70.0004 70.7013 0002902 269.5107 90.5719 14.98328617 07
| Epoch (UTC): | 25 May 2026 12:45:12 |
| Eccentricity: | 0.0002902 |
| inclination: | 70.0004° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 70.7013° |
| argument of perigee: | 269.5107° |
| revolutions per day: | 14.98328617 |
| mean anomaly at epoch: | 90.5719° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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