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 58141U 26145.35764162 +.00000000 +00000-0 +28919-3 0 00006
2 58141 34.9996 128.3131 0005147 176.5463 183.5288 15.23108783 02
| Epoch (UTC): | 25 May 2026 08:35:00 |
| Eccentricity: | 0.0005147 |
| inclination: | 34.9996° |
| perigee height: | 493 km |
| apogee height: | 500 km |
| right ascension of ascending node: | 128.3131° |
| argument of perigee: | 176.5463° |
| revolutions per day: | 15.23108783 |
| mean anomaly at epoch: | 183.5288° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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