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 27056U 26103.94632815 +.00000000 +00000-0 +52718-3 0 00009
2 27056 82.5333 260.9294 0006448 28.1147 131.6303 12.60564621 03
| Epoch (UTC): | 13 April 2026 22:42:42 |
| Eccentricity: | 0.0006448 |
| inclination: | 82.5333° |
| perigee height: | 1416 km |
| apogee height: | 1426 km |
| right ascension of ascending node: | 260.9294° |
| argument of perigee: | 28.1147° |
| revolutions per day: | 12.60564621 |
| mean anomaly at epoch: | 131.6303° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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