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 26137.68248977 +.00000000 +00000-0 +19078-3 0 00001
2 36416 63.3832 126.6771 0696824 3.1400 357.3683 13.73097774 03
| Epoch (UTC): | 17 May 2026 16:22:47 |
| Eccentricity: | 0.0696824 |
| inclination: | 63.3832° |
| perigee height: | 475 km |
| apogee height: | 1502 km |
| right ascension of ascending node: | 126.6771° |
| argument of perigee: | 3.1400° |
| revolutions per day: | 13.73097774 |
| mean anomaly at epoch: | 357.3683° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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