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 46045U 26145.27449399 +.00000000 +00000-0 +14574-4 0 00002
2 46045 53.1593 130.9746 0001443 90.7178 269.3988 15.30193745 04
| Epoch (UTC): | 25 May 2026 06:35:16 |
| Eccentricity: | 0.0001443 |
| inclination: | 53.1593° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 130.9746° |
| argument of perigee: | 90.7178° |
| revolutions per day: | 15.30193745 |
| mean anomaly at epoch: | 269.3988° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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