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 36036U 26145.53385892 +.00000000 +00000-0 +79091-4 0 00002
2 36036 98.4429 333.2008 0001311 92.1529 267.9809 14.39758578 07
| Epoch (UTC): | 25 May 2026 12:48:45 |
| Eccentricity: | 0.0001311 |
| inclination: | 98.4429° |
| perigee height: | 758 km |
| apogee height: | 760 km |
| right ascension of ascending node: | 333.2008° |
| argument of perigee: | 92.1529° |
| revolutions per day: | 14.39758578 |
| mean anomaly at epoch: | 267.9809° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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