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 49112U 26145.62370205 +.00000000 +00000-0 +21576-3 0 00007
2 49112 86.4107 165.8761 0017142 123.5605 236.7179 13.42861834 01
| Epoch (UTC): | 25 May 2026 14:58:07 |
| Eccentricity: | 0.0017142 |
| inclination: | 86.4107° |
| perigee height: | 1086 km |
| apogee height: | 1111 km |
| right ascension of ascending node: | 165.8761° |
| argument of perigee: | 123.5605° |
| revolutions per day: | 13.42861834 |
| mean anomaly at epoch: | 236.7179° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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