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 58138U 26145.47336190 +.00000000 +00000-0 +28114-5 0 00000
2 58138 43.0004 58.5453 0000886 245.9248 114.1511 15.27581537 02
| Epoch (UTC): | 25 May 2026 11:21:38 |
| Eccentricity: | 0.0000886 |
| inclination: | 43.0004° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 58.5453° |
| argument of perigee: | 245.9248° |
| revolutions per day: | 15.27581537 |
| mean anomaly at epoch: | 114.1511° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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