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 55479U 26145.32677022 +.00000000 +00000-0 +16100-4 0 00002
2 55479 43.0025 248.7908 0001400 270.6875 89.3816 15.27576275 06
| Epoch (UTC): | 25 May 2026 07:50:32 |
| Eccentricity: | 0.0001400 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 248.7908° |
| argument of perigee: | 270.6875° |
| revolutions per day: | 15.27576275 |
| mean anomaly at epoch: | 89.3816° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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