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 55358U 26145.50850691 +.00000000 +00000-0 +11990-4 0 00005
2 55358 43.0040 229.4187 0001394 265.7907 94.2785 15.27571986 01
| Epoch (UTC): | 25 May 2026 12:12:14 |
| Eccentricity: | 0.0001394 |
| inclination: | 43.0040° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 229.4187° |
| argument of perigee: | 265.7907° |
| revolutions per day: | 15.27571986 |
| mean anomaly at epoch: | 94.2785° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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