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 26114.20309455 +.00000000 +00000-0 +16326-4 0 00007
2 36795 97.9999 165.0838 0011496 12.8419 347.3083 14.78659551 00
| Epoch (UTC): | 24 April 2026 04:52:27 |
| Eccentricity: | 0.0011496 |
| inclination: | 97.9999° |
| perigee height: | 625 km |
| apogee height: | 642 km |
| right ascension of ascending node: | 165.0838° |
| argument of perigee: | 12.8419° |
| revolutions per day: | 14.78659551 |
| mean anomaly at epoch: | 347.3083° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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