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 45543U 26145.18441801 +.00000000 +00000-0 +12324-2 0 00003
2 45543 53.1566 104.2197 0004298 63.8489 296.2956 15.36424986 01
| Epoch (UTC): | 25 May 2026 04:25:33 |
| Eccentricity: | 0.0004298 |
| inclination: | 53.1566° |
| perigee height: | 454 km |
| apogee height: | 460 km |
| right ascension of ascending node: | 104.2197° |
| argument of perigee: | 63.8489° |
| revolutions per day: | 15.36424986 |
| mean anomaly at epoch: | 296.2956° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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