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 45146U 26145.14891955 +.00000000 +00000-0 +11673-2 0 00003
2 45146 87.8857 40.8541 0002313 74.9473 285.1910 13.10375755 03
| Epoch (UTC): | 25 May 2026 03:34:26 |
| Eccentricity: | 0.0002313 |
| inclination: | 87.8857° |
| perigee height: | 1220 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 40.8541° |
| argument of perigee: | 74.9473° |
| revolutions per day: | 13.10375755 |
| mean anomaly at epoch: | 285.1910° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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