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 49771U 26145.44092847 +.00000000 +00000-0 +14448-3 0 00001
2 49771 53.2113 154.5727 0001211 90.7001 269.4130 15.08831933 04
| Epoch (UTC): | 25 May 2026 10:34:56 |
| Eccentricity: | 0.0001211 |
| inclination: | 53.2113° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 154.5727° |
| argument of perigee: | 90.7001° |
| revolutions per day: | 15.08831933 |
| mean anomaly at epoch: | 269.4130° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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