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 41434U 26144.67539705 +.00000000 +00000-0 +00000-0 0 00008
2 41434 60.1943 38.2721 0057467 232.2820 308.9754 1.00263774 08
| Epoch (UTC): | 24 May 2026 16:12:34 |
| Eccentricity: | 0.0057467 |
| inclination: | 60.1943° |
| perigee height: | 35547 km |
| apogee height: | 36031 km |
| right ascension of ascending node: | 38.2721° |
| argument of perigee: | 232.2820° |
| revolutions per day: | 1.00263774 |
| mean anomaly at epoch: | 308.9754° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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