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 58457U 26145.55392987 +.00000000 +00000-0 +40732-4 0 00008
2 58457 43.0030 327.1948 0001336 276.6950 83.3750 15.27577564 08
| Epoch (UTC): | 25 May 2026 13:17:39 |
| Eccentricity: | 0.0001336 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 327.1948° |
| argument of perigee: | 276.6950° |
| revolutions per day: | 15.27577564 |
| mean anomaly at epoch: | 83.3750° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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