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 36414U 26150.12224582 +.00000000 +00000-0 +14514-3 0 00009
2 36414 63.3678 44.6047 0536818 20.7665 341.4295 13.45706954 07
| Epoch (UTC): | 30 May 2026 02:56:02 |
| Eccentricity: | 0.0536818 |
| inclination: | 63.3678° |
| perigee height: | 687 km |
| apogee height: | 1489 km |
| right ascension of ascending node: | 44.6047° |
| argument of perigee: | 20.7665° |
| revolutions per day: | 13.45706954 |
| mean anomaly at epoch: | 341.4295° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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