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 36416U 26109.20620014 +.00000000 +00000-0 +94236-4 0 00004
2 36416 63.3862 204.1595 0694149 2.9292 357.5499 13.73049656 09
| Epoch (UTC): | 19 April 2026 04:56:55 |
| Eccentricity: | 0.0694149 |
| inclination: | 63.3862° |
| perigee height: | 477 km |
| apogee height: | 1500 km |
| right ascension of ascending node: | 204.1595° |
| argument of perigee: | 2.9292° |
| revolutions per day: | 13.73049656 |
| mean anomaly at epoch: | 357.5499° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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