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 55752U 26145.46438881 +.00000000 +00000-0 -14912-4 0 00009
2 55752 70.0005 50.7472 0002571 269.3888 90.6976 14.98328885 05
| Epoch (UTC): | 25 May 2026 11:08:43 |
| Eccentricity: | 0.0002571 |
| inclination: | 70.0005° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 50.7472° |
| argument of perigee: | 269.3888° |
| revolutions per day: | 14.98328885 |
| mean anomaly at epoch: | 90.6976° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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