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 46142U 26144.80604589 +.00000000 +00000-0 +73511-3 0 00007
2 46142 53.0428 283.6765 0002097 22.2105 337.9002 15.71129117 07
| Epoch (UTC): | 24 May 2026 19:20:42 |
| Eccentricity: | 0.0002097 |
| inclination: | 53.0428° |
| perigee height: | 354 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 283.6765° |
| argument of perigee: | 22.2105° |
| revolutions per day: | 15.71129117 |
| mean anomaly at epoch: | 337.9002° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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