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 46074U 26145.59793133 +.00000000 +00000-0 +12942-2 0 00002
2 46074 53.0508 104.0724 0004077 63.2642 296.8774 15.28160931 02
| Epoch (UTC): | 25 May 2026 14:21:01 |
| Eccentricity: | 0.0004077 |
| inclination: | 53.0508° |
| perigee height: | 479 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 104.0724° |
| argument of perigee: | 63.2642° |
| revolutions per day: | 15.28160931 |
| mean anomaly at epoch: | 296.8774° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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