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 49430U 26145.00307855 +.00000000 +00000-0 +19959-3 0 00005
2 49430 53.2136 246.8142 0001160 85.3834 274.7290 15.08835704 00
| Epoch (UTC): | 25 May 2026 00:04:25 |
| Eccentricity: | 0.0001160 |
| inclination: | 53.2136° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 246.8142° |
| argument of perigee: | 85.3834° |
| revolutions per day: | 15.08835704 |
| mean anomaly at epoch: | 274.7290° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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