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 54023U 26145.44964688 +.00000000 +00000-0 +54526-4 0 00000
2 54023 98.3937 137.5013 0011855 256.2302 103.7569 14.42664938 03
| Epoch (UTC): | 25 May 2026 10:47:29 |
| Eccentricity: | 0.0011855 |
| inclination: | 98.3937° |
| perigee height: | 741 km |
| apogee height: | 758 km |
| right ascension of ascending node: | 137.5013° |
| argument of perigee: | 256.2302° |
| revolutions per day: | 14.42664938 |
| mean anomaly at epoch: | 103.7569° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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