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 55782U 26145.61014883 +.00000000 +00000-0 -59985-5 0 00001
2 55782 70.0002 10.6956 0002638 269.2186 90.8671 14.98329349 01
| Epoch (UTC): | 25 May 2026 14:38:36 |
| Eccentricity: | 0.0002638 |
| inclination: | 70.0002° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 10.6956° |
| argument of perigee: | 269.2186° |
| revolutions per day: | 14.98329349 |
| mean anomaly at epoch: | 90.8671° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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