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 36596U 26158.82344117 +.00000000 +00000-0 +28023-3 0 00002
2 36596 97.7623 176.2940 0008100 122.4026 237.7991 15.16639107 07
| Epoch (UTC): | 07 June 2026 19:45:45 |
| Eccentricity: | 0.0008100 |
| inclination: | 97.7623° |
| perigee height: | 510 km |
| apogee height: | 522 km |
| right ascension of ascending node: | 176.2940° |
| argument of perigee: | 122.4026° |
| revolutions per day: | 15.16639107 |
| mean anomaly at epoch: | 237.7991° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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