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 55333U 26145.53402399 +.00000000 +00000-0 +21335-2 0 00001
2 55333 43.0003 229.6162 0001477 270.9520 89.1162 15.27226226 05
| Epoch (UTC): | 25 May 2026 12:48:59 |
| Eccentricity: | 0.0001477 |
| inclination: | 43.0003° |
| perigee height: | 483 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 229.6162° |
| argument of perigee: | 270.9520° |
| revolutions per day: | 15.27226226 |
| mean anomaly at epoch: | 89.1162° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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