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 41944U 26145.60710612 +.00000000 +00000-0 +00000-0 0 00006
2 41944 0.0183 287.7532 0002365 138.4620 153.5417 1.00271488 07
| Epoch (UTC): | 25 May 2026 14:34:13 |
| Eccentricity: | 0.0002365 |
| inclination: | 0.0183° |
| perigee height: | 35777 km |
| apogee height: | 35797 km |
| right ascension of ascending node: | 287.7532° |
| argument of perigee: | 138.4620° |
| revolutions per day: | 1.00271488 |
| mean anomaly at epoch: | 153.5417° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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