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 36112U 26144.45920227 +.00000000 +00000-0 +00000-0 0 00004
2 36112 64.9840 71.6253 0001878 127.8852 52.6374 2.13100931 04
| Epoch (UTC): | 24 May 2026 11:01:15 |
| Eccentricity: | 0.0001878 |
| inclination: | 64.9840° |
| perigee height: | 19125 km |
| apogee height: | 19135 km |
| right ascension of ascending node: | 71.6253° |
| argument of perigee: | 127.8852° |
| revolutions per day: | 2.13100931 |
| mean anomaly at epoch: | 52.6374° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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