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 46355U 26144.93139038 +.00000000 +00000-0 +13347-2 0 00009
2 46355 53.1561 15.1873 0004579 129.8885 230.2521 15.36658201 09
| Epoch (UTC): | 24 May 2026 22:21:12 |
| Eccentricity: | 0.0004579 |
| inclination: | 53.1561° |
| perigee height: | 453 km |
| apogee height: | 459 km |
| right ascension of ascending node: | 15.1873° |
| argument of perigee: | 129.8885° |
| revolutions per day: | 15.36658201 |
| mean anomaly at epoch: | 230.2521° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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