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 41469U 26145.32418985 +.00000000 +00000-0 +00000-0 0 00005
2 41469 5.1414 98.0026 0007325 348.7936 42.2920 1.00277583 05
| Epoch (UTC): | 25 May 2026 07:46:50 |
| Eccentricity: | 0.0007325 |
| inclination: | 5.1414° |
| perigee height: | 35754 km |
| apogee height: | 35816 km |
| right ascension of ascending node: | 98.0026° |
| argument of perigee: | 348.7936° |
| revolutions per day: | 1.00277583 |
| mean anomaly at epoch: | 42.2920° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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