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 55756U 26145.45604242 +.00000000 +00000-0 -15293-4 0 00001
2 55756 70.0007 50.7170 0002619 266.9499 93.1361 14.98327766 03
| Epoch (UTC): | 25 May 2026 10:56:42 |
| Eccentricity: | 0.0002619 |
| inclination: | 70.0007° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 50.7170° |
| argument of perigee: | 266.9499° |
| revolutions per day: | 14.98327766 |
| mean anomaly at epoch: | 93.1361° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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