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 27059U 26104.18792102 +.00000000 +00000-0 -17577-3 0 00000
2 27059 82.5377 253.7232 0002651 55.9498 304.1844 12.61555901 04
| Epoch (UTC): | 14 April 2026 04:30:36 |
| Eccentricity: | 0.0002651 |
| inclination: | 82.5377° |
| perigee height: | 1414 km |
| apogee height: | 1419 km |
| right ascension of ascending node: | 253.7232° |
| argument of perigee: | 55.9498° |
| revolutions per day: | 12.61555901 |
| mean anomaly at epoch: | 304.1844° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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