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 36519U 26106.62568659 +.00000000 +00000-0 +44662-4 0 00005
2 36519 82.9570 294.9509 0035002 302.0782 125.5139 13.71661697 00
| Epoch (UTC): | 16 April 2026 15:00:59 |
| Eccentricity: | 0.0035002 |
| inclination: | 82.9570° |
| perigee height: | 968 km |
| apogee height: | 1019 km |
| right ascension of ascending node: | 294.9509° |
| argument of perigee: | 302.0782° |
| revolutions per day: | 13.71661697 |
| mean anomaly at epoch: | 125.5139° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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