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 48424U 26145.48356418 +.00000000 +00000-0 +13672-3 0 00004
2 48424 34.9940 169.4161 0004405 337.8279 22.2238 15.02576108 07
| Epoch (UTC): | 25 May 2026 11:36:19 |
| Eccentricity: | 0.0004405 |
| inclination: | 34.9940° |
| perigee height: | 556 km |
| apogee height: | 562 km |
| right ascension of ascending node: | 169.4161° |
| argument of perigee: | 337.8279° |
| revolutions per day: | 15.02576108 |
| mean anomaly at epoch: | 22.2238° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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