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 41036U 26145.58069508 +.00000000 +00000-0 +00000-0 0 00006
2 41036 0.0399 115.3357 0002430 303.7576 18.1267 1.00271712 08
| Epoch (UTC): | 25 May 2026 13:56:12 |
| Eccentricity: | 0.0002430 |
| inclination: | 0.0399° |
| perigee height: | 35776 km |
| apogee height: | 35797 km |
| right ascension of ascending node: | 115.3357° |
| argument of perigee: | 303.7576° |
| revolutions per day: | 1.00271712 |
| mean anomaly at epoch: | 18.1267° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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