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 43441U 26145.58941031 +.00000000 +00000-0 +28313-3 0 00008
2 43441 97.0390 171.0811 0007718 320.7030 39.3648 15.25497984 00
| Epoch (UTC): | 25 May 2026 14:08:45 |
| Eccentricity: | 0.0007718 |
| inclination: | 97.0390° |
| perigee height: | 484 km |
| apogee height: | 495 km |
| right ascension of ascending node: | 171.0811° |
| argument of perigee: | 320.7030° |
| revolutions per day: | 15.25497984 |
| mean anomaly at epoch: | 39.3648° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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