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 26041.86415109 +.00000000 +00000-0 +66026-4 0 00009
2 14974 82.9384 310.7014 0045355 153.6538 276.3463 13.77163518 03
| Epoch (UTC): | 10 February 2026 20:44:22 |
| Eccentricity: | 0.0045355 |
| inclination: | 82.9384° |
| perigee height: | 941 km |
| apogee height: | 1007 km |
| right ascension of ascending node: | 310.7014° |
| argument of perigee: | 153.6538° |
| revolutions per day: | 13.77163518 |
| mean anomaly at epoch: | 276.3463° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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