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 43678U 26145.62854044 +.00000000 +00000-0 +18494-3 0 00001
2 43678 98.1138 340.8647 0011607 247.2872 112.7124 15.00326831 06
| Epoch (UTC): | 25 May 2026 15:05:05 |
| Eccentricity: | 0.0011607 |
| inclination: | 98.1138° |
| perigee height: | 558 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 340.8647° |
| argument of perigee: | 247.2872° |
| revolutions per day: | 15.00326831 |
| mean anomaly at epoch: | 112.7124° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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