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 36032U 26145.59508182 +.00000000 +00000-0 +00000-0 0 00003
2 36032 0.0729 66.8731 0005092 327.1448 120.4002 1.00273607 05
| Epoch (UTC): | 25 May 2026 14:16:55 |
| Eccentricity: | 0.0005092 |
| inclination: | 0.0729° |
| perigee height: | 35765 km |
| apogee height: | 35808 km |
| right ascension of ascending node: | 66.8731° |
| argument of perigee: | 327.1448° |
| revolutions per day: | 1.00273607 |
| mean anomaly at epoch: | 120.4002° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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