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 49426U 26144.99104885 +.00000000 +00000-0 +41069-4 0 00003
2 49426 53.2148 246.5902 0001152 86.8016 273.3108 15.08837658 01
| Epoch (UTC): | 24 May 2026 23:47:06 |
| Eccentricity: | 0.0001152 |
| inclination: | 53.2148° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 246.5902° |
| argument of perigee: | 86.8016° |
| revolutions per day: | 15.08837658 |
| mean anomaly at epoch: | 273.3108° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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