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 27057U 26104.17239255 +.00000000 +00000-0 +33670-4 0 00004
2 27057 82.5410 255.1418 0000895 124.5184 235.5991 12.61615584 09
| Epoch (UTC): | 14 April 2026 04:08:14 |
| Eccentricity: | 0.0000895 |
| inclination: | 82.5410° |
| perigee height: | 1416 km |
| apogee height: | 1417 km |
| right ascension of ascending node: | 255.1418° |
| argument of perigee: | 124.5184° |
| revolutions per day: | 12.61615584 |
| mean anomaly at epoch: | 235.5991° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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