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 36516U 26145.56370833 +.00000000 +00000-0 +00000-0 0 00007
2 36516 0.0149 315.2546 0002761 109.0036 280.8205 1.00272067 08
| Epoch (UTC): | 25 May 2026 13:31:44 |
| Eccentricity: | 0.0002761 |
| inclination: | 0.0149° |
| perigee height: | 35775 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 315.2546° |
| argument of perigee: | 109.0036° |
| revolutions per day: | 1.00272067 |
| mean anomaly at epoch: | 280.8205° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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