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 43642U 26145.62449958 +.00000000 +00000-0 +12534-3 0 00005
2 43642 98.1492 174.4400 0001139 98.1683 261.9648 14.63139380 07
| Epoch (UTC): | 25 May 2026 14:59:16 |
| Eccentricity: | 0.0001139 |
| inclination: | 98.1492° |
| perigee height: | 682 km |
| apogee height: | 684 km |
| right ascension of ascending node: | 174.4400° |
| argument of perigee: | 98.1683° |
| revolutions per day: | 14.63139380 |
| mean anomaly at epoch: | 261.9648° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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