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 00424U 26077.08995411 +.00000000 +00000-0 +11436-3 0 00000
2 00424 80.4709 346.5389 0023577 110.5619 249.8060 13.69574519 04
| Epoch (UTC): | 18 March 2026 02:09:32 |
| Eccentricity: | 0.0023577 |
| inclination: | 80.4709° |
| perigee height: | 984 km |
| apogee height: | 1018 km |
| right ascension of ascending node: | 346.5389° |
| argument of perigee: | 110.5619° |
| revolutions per day: | 13.69574519 |
| mean anomaly at epoch: | 249.8060° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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