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 46329U 26145.48165154 +.00000000 +00000-0 +78880-3 0 00003
2 46329 53.0431 321.0786 0002083 124.4960 235.6253 15.69235369 03
| Epoch (UTC): | 25 May 2026 11:33:34 |
| Eccentricity: | 0.0002083 |
| inclination: | 53.0431° |
| perigee height: | 360 km |
| apogee height: | 362 km |
| right ascension of ascending node: | 321.0786° |
| argument of perigee: | 124.4960° |
| revolutions per day: | 15.69235369 |
| mean anomaly at epoch: | 235.6253° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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