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 43648U 26145.06019586 +.00000000 +00000-0 +00000-0 0 00001
2 43648 54.1099 300.7961 0004905 55.2566 304.7662 1.86232106 05
| Epoch (UTC): | 25 May 2026 01:26:40 |
| Eccentricity: | 0.0004905 |
| inclination: | 54.1099° |
| perigee height: | 21514 km |
| apogee height: | 21542 km |
| right ascension of ascending node: | 300.7961° |
| argument of perigee: | 55.2566° |
| revolutions per day: | 1.86232106 |
| mean anomaly at epoch: | 304.7662° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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