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 55495U 26145.58060830 +.00000000 +00000-0 +28999-4 0 00000
2 55495 43.0031 247.2602 0001305 253.7053 106.3655 15.27578901 09
| Epoch (UTC): | 25 May 2026 13:56:04 |
| Eccentricity: | 0.0001305 |
| inclination: | 43.0031° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 247.2602° |
| argument of perigee: | 253.7053° |
| revolutions per day: | 15.27578901 |
| mean anomaly at epoch: | 106.3655° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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