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 40536U 26145.63221235 +.00000000 +00000-0 +34468-3 0 00001
2 40536 97.6887 135.3647 0054961 258.2876 101.2206 15.52864289 09
| Epoch (UTC): | 25 May 2026 15:10:23 |
| Eccentricity: | 0.0054961 |
| inclination: | 97.6887° |
| perigee height: | 371 km |
| apogee height: | 446 km |
| right ascension of ascending node: | 135.3647° |
| argument of perigee: | 258.2876° |
| revolutions per day: | 15.52864289 |
| mean anomaly at epoch: | 101.2206° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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