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 41026U 26145.65323867 +.00000000 +00000-0 +24533-3 0 00004
2 41026 97.3040 284.3838 0009178 269.7884 90.2303 15.27081228 06
| Epoch (UTC): | 25 May 2026 15:40:39 |
| Eccentricity: | 0.0009178 |
| inclination: | 97.3040° |
| perigee height: | 478 km |
| apogee height: | 491 km |
| right ascension of ascending node: | 284.3838° |
| argument of perigee: | 269.7884° |
| revolutions per day: | 15.27081228 |
| mean anomaly at epoch: | 90.2303° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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