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 55744U 26145.17666916 +.00000000 +00000-0 -15760-4 0 00002
2 55744 70.0010 51.7501 0003035 267.7256 92.3556 14.98324458 08
| Epoch (UTC): | 25 May 2026 04:14:24 |
| Eccentricity: | 0.0003035 |
| inclination: | 70.0010° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 51.7501° |
| argument of perigee: | 267.7256° |
| revolutions per day: | 14.98324458 |
| mean anomaly at epoch: | 92.3556° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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