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 26042.24811500 +.00000000 +00000-0 +64413-4 0 00005
2 14974 82.9384 310.4158 0045376 152.5962 19.9405 13.77163551 05
| Epoch (UTC): | 11 February 2026 05:57:17 |
| Eccentricity: | 0.0045376 |
| inclination: | 82.9384° |
| perigee height: | 941 km |
| apogee height: | 1007 km |
| right ascension of ascending node: | 310.4158° |
| argument of perigee: | 152.5962° |
| revolutions per day: | 13.77163551 |
| mean anomaly at epoch: | 19.9405° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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