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 49451U 26145.51820542 +.00000000 +00000-0 +28690-4 0 00000
2 49451 53.2145 234.2231 0000947 78.4155 281.6943 15.08839478 08
| Epoch (UTC): | 25 May 2026 12:26:12 |
| Eccentricity: | 0.0000947 |
| inclination: | 53.2145° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 234.2231° |
| argument of perigee: | 78.4155° |
| revolutions per day: | 15.08839478 |
| mean anomaly at epoch: | 281.6943° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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