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 26041.92236588 +.00000000 +00000-0 +54550-4 0 00006
2 36519 82.9644 342.4896 0037308 119.2448 304.8264 13.71655275 04
| Epoch (UTC): | 10 February 2026 22:08:12 |
| Eccentricity: | 0.0037308 |
| inclination: | 82.9644° |
| perigee height: | 966 km |
| apogee height: | 1021 km |
| right ascension of ascending node: | 342.4896° |
| argument of perigee: | 119.2448° |
| revolutions per day: | 13.71655275 |
| mean anomaly at epoch: | 304.8264° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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