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 43108U 26143.59550955 +.00000000 +00000-0 +00000-0 0 00008
2 43108 54.3440 303.1537 0002126 272.4030 87.5525 1.86230755 08
| Epoch (UTC): | 23 May 2026 14:17:32 |
| Eccentricity: | 0.0002126 |
| inclination: | 54.3440° |
| perigee height: | 21522 km |
| apogee height: | 21534 km |
| right ascension of ascending node: | 303.1537° |
| argument of perigee: | 272.4030° |
| revolutions per day: | 1.86230755 |
| mean anomaly at epoch: | 87.5525° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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