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 19274U 26044.71178720 +.00000000 +00000-0 +27414-3 0 00006
2 19274 82.4705 287.3169 0011294 259.0727 100.9244 15.31168772 07
| Epoch (UTC): | 13 February 2026 17:04:58 |
| Eccentricity: | 0.0011294 |
| inclination: | 82.4705° |
| perigee height: | 465 km |
| apogee height: | 480 km |
| right ascension of ascending node: | 287.3169° |
| argument of perigee: | 259.0727° |
| revolutions per day: | 15.31168772 |
| mean anomaly at epoch: | 100.9244° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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