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 54848U 26145.41455132 +.00000000 +00000-0 -38465-4 0 00006
2 54848 43.0030 48.3742 0001113 240.9257 119.1483 15.27562775 08
| Epoch (UTC): | 25 May 2026 09:56:57 |
| Eccentricity: | 0.0001113 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 48.3742° |
| argument of perigee: | 240.9257° |
| revolutions per day: | 15.27562775 |
| mean anomaly at epoch: | 119.1483° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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