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 57422U 26144.27001190 +.00000000 +00000-0 +20140-4 0 00001
2 57422 96.1620 190.7721 0023588 129.1661 231.1726 16.07670290 05
| Epoch (UTC): | 24 May 2026 06:28:49 |
| Eccentricity: | 0.0023588 |
| inclination: | 96.1620° |
| perigee height: | 238 km |
| apogee height: | 269 km |
| right ascension of ascending node: | 190.7721° |
| argument of perigee: | 129.1661° |
| revolutions per day: | 16.07670290 |
| mean anomaly at epoch: | 231.1726° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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