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 26041.18272243 +.00000000 +00000-0 +32436-3 0 00009
2 19274 82.4702 290.8992 0011264 274.2882 85.7072 15.31098498 01
| Epoch (UTC): | 10 February 2026 04:23:07 |
| Eccentricity: | 0.0011264 |
| inclination: | 82.4702° |
| perigee height: | 465 km |
| apogee height: | 480 km |
| right ascension of ascending node: | 290.8992° |
| argument of perigee: | 274.2882° |
| revolutions per day: | 15.31098498 |
| mean anomaly at epoch: | 85.7072° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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