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 46173U 26145.61774602 +.00000000 +00000-0 +76580-3 0 00004
2 46173 53.0429 283.2118 0002177 359.8133 0.2881 15.68999727 02
| Epoch (UTC): | 25 May 2026 14:49:33 |
| Eccentricity: | 0.0002177 |
| inclination: | 53.0429° |
| perigee height: | 360 km |
| apogee height: | 363 km |
| right ascension of ascending node: | 283.2118° |
| argument of perigee: | 359.8133° |
| revolutions per day: | 15.68999727 |
| mean anomaly at epoch: | 0.2881° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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