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 46035U 26145.36930529 +.00000000 +00000-0 +18968-4 0 00002
2 46035 53.1596 130.5399 0001197 89.3629 270.7508 15.30191909 01
| Epoch (UTC): | 25 May 2026 08:51:47 |
| Eccentricity: | 0.0001197 |
| inclination: | 53.1596° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 130.5399° |
| argument of perigee: | 89.3629° |
| revolutions per day: | 15.30191909 |
| mean anomaly at epoch: | 270.7508° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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