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 55493U 26145.03600317 +.00000000 +00000-0 +30979-4 0 00009
2 55493 43.0008 268.3746 0001309 277.4752 82.5951 15.27575552 00
| Epoch (UTC): | 25 May 2026 00:51:50 |
| Eccentricity: | 0.0001309 |
| inclination: | 43.0008° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 268.3746° |
| argument of perigee: | 277.4752° |
| revolutions per day: | 15.27575552 |
| mean anomaly at epoch: | 82.5951° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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