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 14974U 26039.25752361 +.00000000 +00000-0 +74090-4 0 00003
2 14974 82.9389 312.6407 0045179 160.9158 313.2757 13.77163097 07
| Epoch (UTC): | 08 February 2026 06:10:50 |
| Eccentricity: | 0.0045179 |
| inclination: | 82.9389° |
| perigee height: | 941 km |
| apogee height: | 1007 km |
| right ascension of ascending node: | 312.6407° |
| argument of perigee: | 160.9158° |
| revolutions per day: | 13.77163097 |
| mean anomaly at epoch: | 313.2757° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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