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 43676U 26145.60044992 +.00000000 +00000-0 +10108-3 0 00004
2 43676 98.0730 327.1258 0006960 164.8287 195.3146 15.01176591 05
| Epoch (UTC): | 25 May 2026 14:24:38 |
| Eccentricity: | 0.0006960 |
| inclination: | 98.0730° |
| perigee height: | 558 km |
| apogee height: | 568 km |
| right ascension of ascending node: | 327.1258° |
| argument of perigee: | 164.8287° |
| revolutions per day: | 15.01176591 |
| mean anomaly at epoch: | 195.3146° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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