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 48274U 26049.89676066 +.00000000 +00000-0 +28199-3 0 00009
2 48274 41.4677 322.4399 0004426 139.3790 220.7380 15.59851583 08
| Epoch (UTC): | 18 February 2026 21:31:20 |
| Eccentricity: | 0.0004426 |
| inclination: | 41.4677° |
| perigee height: | 385 km |
| apogee height: | 391 km |
| right ascension of ascending node: | 322.4399° |
| argument of perigee: | 139.3790° |
| revolutions per day: | 15.59851583 |
| mean anomaly at epoch: | 220.7380° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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