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 49211U 26144.95339611 +.00000000 +00000-0 +94230-3 0 00005
2 49211 87.8947 324.8490 0001697 102.3095 257.8224 13.13468923 05
| Epoch (UTC): | 24 May 2026 22:52:53 |
| Eccentricity: | 0.0001697 |
| inclination: | 87.8947° |
| perigee height: | 1208 km |
| apogee height: | 1211 km |
| right ascension of ascending node: | 324.8490° |
| argument of perigee: | 102.3095° |
| revolutions per day: | 13.13468923 |
| mean anomaly at epoch: | 257.8224° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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