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 46343U 26145.58335647 +.00000000 +00000-0 +81974-3 0 00004
2 46343 53.0312 292.5027 0007882 279.7644 191.1009 15.92366252 09
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0007882 |
| inclination: | 53.0312° |
| perigee height: | 290 km |
| apogee height: | 301 km |
| right ascension of ascending node: | 292.5027° |
| argument of perigee: | 279.7644° |
| revolutions per day: | 15.92366252 |
| mean anomaly at epoch: | 191.1009° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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