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 26040.84602855 +.00000000 +00000-0 +67661-4 0 00008
2 14974 82.9386 311.4589 0045286 156.4872 268.7272 13.77163352 04
| Epoch (UTC): | 09 February 2026 20:18:16 |
| Eccentricity: | 0.0045286 |
| inclination: | 82.9386° |
| perigee height: | 941 km |
| apogee height: | 1007 km |
| right ascension of ascending node: | 311.4589° |
| argument of perigee: | 156.4872° |
| revolutions per day: | 13.77163352 |
| mean anomaly at epoch: | 268.7272° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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