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 26110.25618402 +.00000000 +00000-0 +79443-4 0 00002
2 00424 80.4656 313.7211 0023303 27.8440 332.3948 13.69581036 09
| Epoch (UTC): | 20 April 2026 06:08:54 |
| Eccentricity: | 0.0023303 |
| inclination: | 80.4656° |
| perigee height: | 984 km |
| apogee height: | 1018 km |
| right ascension of ascending node: | 313.7211° |
| argument of perigee: | 27.8440° |
| revolutions per day: | 13.69581036 |
| mean anomaly at epoch: | 332.3948° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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