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 63041U 26145.35347374 +.00000000 +00000-0 +72934-3 0 00009
2 63041 53.1573 262.0800 0001746 78.0274 282.0922 15.30210944 08
| Epoch (UTC): | 25 May 2026 08:29:00 |
| Eccentricity: | 0.0001746 |
| inclination: | 53.1573° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 262.0800° |
| argument of perigee: | 78.0274° |
| revolutions per day: | 15.30210944 |
| mean anomaly at epoch: | 282.0922° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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