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 45048U 26145.41177185 +.00000000 +00000-0 +15732-2 0 00006
2 45048 53.0265 230.6068 0007335 21.4248 338.7067 15.54807890 09
| Epoch (UTC): | 25 May 2026 09:52:57 |
| Eccentricity: | 0.0007335 |
| inclination: | 53.0265° |
| perigee height: | 398 km |
| apogee height: | 408 km |
| right ascension of ascending node: | 230.6068° |
| argument of perigee: | 21.4248° |
| revolutions per day: | 15.54807890 |
| mean anomaly at epoch: | 338.7067° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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