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 46275U 26145.64037400 +.00000000 +00000-0 +25837-3 0 00007
2 46275 97.1923 210.0598 0002543 102.8934 257.2601 15.48321977 03
| Epoch (UTC): | 25 May 2026 15:22:08 |
| Eccentricity: | 0.0002543 |
| inclination: | 97.1923° |
| perigee height: | 420 km |
| apogee height: | 423 km |
| right ascension of ascending node: | 210.0598° |
| argument of perigee: | 102.8934° |
| revolutions per day: | 15.48321977 |
| mean anomaly at epoch: | 257.2601° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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