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 48367U 26145.56899735 +.00000000 +00000-0 +78569-4 0 00000
2 48367 53.1608 347.8294 0001203 83.8157 276.2981 15.31702074 03
| Epoch (UTC): | 25 May 2026 13:39:21 |
| Eccentricity: | 0.0001203 |
| inclination: | 53.1608° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 347.8294° |
| argument of perigee: | 83.8157° |
| revolutions per day: | 15.31702074 |
| mean anomaly at epoch: | 276.2981° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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