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 26048.37976803 +.00000000 +00000-0 +80557-4 0 00005
2 00424 80.4682 14.9407 0022563 183.6495 176.4490 13.69568789 02
| Epoch (UTC): | 17 February 2026 09:06:51 |
| Eccentricity: | 0.0022563 |
| inclination: | 80.4682° |
| perigee height: | 984 km |
| apogee height: | 1018 km |
| right ascension of ascending node: | 14.9407° |
| argument of perigee: | 183.6495° |
| revolutions per day: | 13.69568789 |
| mean anomaly at epoch: | 176.4490° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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