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 26039.82801520 +.00000000 +00000-0 +68107-4 0 00000
2 14974 82.9388 312.2163 0045220 159.3322 261.6380 13.77163174 07
| Epoch (UTC): | 08 February 2026 19:52:20 |
| Eccentricity: | 0.0045220 |
| inclination: | 82.9388° |
| perigee height: | 941 km |
| apogee height: | 1007 km |
| right ascension of ascending node: | 312.2163° |
| argument of perigee: | 159.3322° |
| revolutions per day: | 13.77163174 |
| mean anomaly at epoch: | 261.6380° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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