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 00058U 26129.85409869 +.00000000 +00000-0 +28412-4 0 00006
2 00058 28.3302 334.2408 0164933 250.3829 107.8844 13.46429169 09
| Epoch (UTC): | 09 May 2026 20:29:54 |
| Eccentricity: | 0.0164933 |
| inclination: | 28.3302° |
| perigee height: | 962 km |
| apogee height: | 1209 km |
| right ascension of ascending node: | 334.2408° |
| argument of perigee: | 250.3829° |
| revolutions per day: | 13.46429169 |
| mean anomaly at epoch: | 107.8844° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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