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 37256U 26141.72681502 +.00000000 +00000-0 +00000-0 0 00001
2 37256 47.5987 272.1591 0054474 211.8397 123.6506 1.00291558 01
| Epoch (UTC): | 21 May 2026 17:26:36 |
| Eccentricity: | 0.0054474 |
| inclination: | 47.5987° |
| perigee height: | 35551 km |
| apogee height: | 36011 km |
| right ascension of ascending node: | 272.1591° |
| argument of perigee: | 211.8397° |
| revolutions per day: | 1.00291558 |
| mean anomaly at epoch: | 123.6506° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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