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 45462U 26145.66344588 +.00000000 +00000-0 +19952-3 0 00005
2 45462 34.9966 345.8111 0001732 236.7544 123.2998 15.02596673 05
| Epoch (UTC): | 25 May 2026 15:55:21 |
| Eccentricity: | 0.0001732 |
| inclination: | 34.9966° |
| perigee height: | 558 km |
| apogee height: | 560 km |
| right ascension of ascending node: | 345.8111° |
| argument of perigee: | 236.7544° |
| revolutions per day: | 15.02596673 |
| mean anomaly at epoch: | 123.2998° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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