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 55648U 26145.28427689 +.00000000 +00000-0 -65689-3 0 00003
2 55648 69.9992 351.3706 0002745 267.4792 92.6052 14.98368448 03
| Epoch (UTC): | 25 May 2026 06:49:21 |
| Eccentricity: | 0.0002745 |
| inclination: | 69.9992° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 351.3706° |
| argument of perigee: | 267.4792° |
| revolutions per day: | 14.98368448 |
| mean anomaly at epoch: | 92.6052° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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