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 62424U 26145.35074985 +.00000000 +00000-0 +83231-3 0 00000
2 62424 42.9995 252.7632 0001473 318.3587 41.7152 15.27584656 04
| Epoch (UTC): | 25 May 2026 08:25:04 |
| Eccentricity: | 0.0001473 |
| inclination: | 42.9995° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 252.7632° |
| argument of perigee: | 318.3587° |
| revolutions per day: | 15.27584656 |
| mean anomaly at epoch: | 41.7152° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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