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 54020U 26145.53676884 +.00000000 +00000-0 +17323-3 0 00008
2 54020 54.9995 303.5967 0013431 29.2784 330.8960 14.62966241 01
| Epoch (UTC): | 25 May 2026 12:52:56 |
| Eccentricity: | 0.0013431 |
| inclination: | 54.9995° |
| perigee height: | 674 km |
| apogee height: | 693 km |
| right ascension of ascending node: | 303.5967° |
| argument of perigee: | 29.2784° |
| revolutions per day: | 14.62966241 |
| mean anomaly at epoch: | 330.8960° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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