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 58455U 26145.53479772 +.00000000 +00000-0 +21448-3 0 00004
2 58455 43.0014 327.9048 0001102 277.1255 82.9471 15.27588039 06
| Epoch (UTC): | 25 May 2026 12:50:06 |
| Eccentricity: | 0.0001102 |
| inclination: | 43.0014° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 327.9048° |
| argument of perigee: | 277.1255° |
| revolutions per day: | 15.27588039 |
| mean anomaly at epoch: | 82.9471° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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