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 45686U 26145.05904740 +.00000000 +00000-0 +11545-2 0 00007
2 45686 53.1586 50.8220 0004969 111.4124 248.7412 15.42723270 09
| Epoch (UTC): | 25 May 2026 01:25:01 |
| Eccentricity: | 0.0004969 |
| inclination: | 53.1586° |
| perigee height: | 435 km |
| apogee height: | 441 km |
| right ascension of ascending node: | 50.8220° |
| argument of perigee: | 111.4124° |
| revolutions per day: | 15.42723270 |
| mean anomaly at epoch: | 248.7412° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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