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 46061U 26145.33500095 +.00000000 +00000-0 +25697-5 0 00007
2 46061 53.1602 117.4033 0001084 85.2072 274.9054 15.31704655 00
| Epoch (UTC): | 25 May 2026 08:02:24 |
| Eccentricity: | 0.0001084 |
| inclination: | 53.1602° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 117.4033° |
| argument of perigee: | 85.2072° |
| revolutions per day: | 15.31704655 |
| mean anomaly at epoch: | 274.9054° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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