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 43677U 26145.08704637 +.00000000 +00000-0 +18225-3 0 00004
2 43677 98.0756 336.4779 0009374 191.9139 168.1864 15.02811720 00
| Epoch (UTC): | 25 May 2026 02:05:20 |
| Eccentricity: | 0.0009374 |
| inclination: | 98.0756° |
| perigee height: | 552 km |
| apogee height: | 565 km |
| right ascension of ascending node: | 336.4779° |
| argument of perigee: | 191.9139° |
| revolutions per day: | 15.02811720 |
| mean anomaly at epoch: | 168.1864° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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