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 45671U 26145.12375903 +.00000000 +00000-0 +51301-3 0 00007
2 45671 53.0438 41.3281 0002958 46.7954 313.3307 15.64978762 01
| Epoch (UTC): | 25 May 2026 02:58:12 |
| Eccentricity: | 0.0002958 |
| inclination: | 53.0438° |
| perigee height: | 371 km |
| apogee height: | 375 km |
| right ascension of ascending node: | 41.3281° |
| argument of perigee: | 46.7954° |
| revolutions per day: | 15.64978762 |
| mean anomaly at epoch: | 313.3307° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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