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 43811U 26145.57405646 +.00000000 +00000-0 +15532-3 0 00004
2 43811 97.4087 189.0833 0013746 59.6946 300.5641 15.08482728 00
| Epoch (UTC): | 25 May 2026 13:46:38 |
| Eccentricity: | 0.0013746 |
| inclination: | 97.4087° |
| perigee height: | 531 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 189.0833° |
| argument of perigee: | 59.6946° |
| revolutions per day: | 15.08482728 |
| mean anomaly at epoch: | 300.5641° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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