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 63046U 26145.58518775 +.00000000 +00000-0 +54848-3 0 00008
2 63046 53.1614 260.6822 0000997 305.9933 54.0975 15.30174927 03
| Epoch (UTC): | 25 May 2026 14:02:40 |
| Eccentricity: | 0.0000997 |
| inclination: | 53.1614° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 260.6822° |
| argument of perigee: | 305.9933° |
| revolutions per day: | 15.30174927 |
| mean anomaly at epoch: | 54.0975° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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