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 45223U 26145.62350780 +.00000000 +00000-0 +47815-3 0 00006
2 45223 53.0410 335.5562 0003411 107.5412 252.5975 15.65557508 01
| Epoch (UTC): | 25 May 2026 14:57:51 |
| Eccentricity: | 0.0003411 |
| inclination: | 53.0410° |
| perigee height: | 369 km |
| apogee height: | 374 km |
| right ascension of ascending node: | 335.5562° |
| argument of perigee: | 107.5412° |
| revolutions per day: | 15.65557508 |
| mean anomaly at epoch: | 252.5975° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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