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 46497U 26145.57779837 +.00000000 +00000-0 +18798-3 0 00000
2 46497 98.0979 138.1726 0007861 153.1278 207.0356 15.04383208 08
| Epoch (UTC): | 25 May 2026 13:52:01 |
| Eccentricity: | 0.0007861 |
| inclination: | 98.0979° |
| perigee height: | 548 km |
| apogee height: | 559 km |
| right ascension of ascending node: | 138.1726° |
| argument of perigee: | 153.1278° |
| revolutions per day: | 15.04383208 |
| mean anomaly at epoch: | 207.0356° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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