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 43915U 26145.58387175 +.00000000 +00000-0 +15626-3 0 00000
2 43915 50.0124 323.5985 0006938 246.6572 113.3614 14.29019357 09
| Epoch (UTC): | 25 May 2026 14:00:46 |
| Eccentricity: | 0.0006938 |
| inclination: | 50.0124° |
| perigee height: | 790 km |
| apogee height: | 800 km |
| right ascension of ascending node: | 323.5985° |
| argument of perigee: | 246.6572° |
| revolutions per day: | 14.29019357 |
| mean anomaly at epoch: | 113.3614° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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