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 36795U 26063.18017050 +.00000000 +00000-0 +10786-3 0 00007
2 36795 97.8563 114.5815 0011532 166.2623 193.8904 14.78666685 04
| Epoch (UTC): | 04 March 2026 04:19:26 |
| Eccentricity: | 0.0011532 |
| inclination: | 97.8563° |
| perigee height: | 625 km |
| apogee height: | 642 km |
| right ascension of ascending node: | 114.5815° |
| argument of perigee: | 166.2623° |
| revolutions per day: | 14.78666685 |
| mean anomaly at epoch: | 193.8904° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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