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 41549U 26143.15990341 +.00000000 +00000-0 +00000-0 0 00004
2 41549 55.1018 222.3833 0002676 335.5312 24.5109 1.70474082 05
| Epoch (UTC): | 23 May 2026 03:50:15 |
| Eccentricity: | 0.0002676 |
| inclination: | 55.1018° |
| perigee height: | 23214 km |
| apogee height: | 23230 km |
| right ascension of ascending node: | 222.3833° |
| argument of perigee: | 335.5312° |
| revolutions per day: | 1.70474082 |
| mean anomaly at epoch: | 24.5109° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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