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 49114U 26145.53880118 +.00000000 +00000-0 +36812-3 0 00007
2 49114 86.4107 165.8873 0020748 121.9527 238.3639 13.42858513 07
| Epoch (UTC): | 25 May 2026 12:55:52 |
| Eccentricity: | 0.0020748 |
| inclination: | 86.4107° |
| perigee height: | 1083 km |
| apogee height: | 1114 km |
| right ascension of ascending node: | 165.8873° |
| argument of perigee: | 121.9527° |
| revolutions per day: | 13.42858513 |
| mean anomaly at epoch: | 238.3639° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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