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 49727U 26145.46852698 +.00000000 +00000-0 +25410-4 0 00004
2 49727 53.2105 174.4494 0000945 66.5691 293.5400 15.08840399 01
| Epoch (UTC): | 25 May 2026 11:14:40 |
| Eccentricity: | 0.0000945 |
| inclination: | 53.2105° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 174.4494° |
| argument of perigee: | 66.5691° |
| revolutions per day: | 15.08840399 |
| mean anomaly at epoch: | 293.5400° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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