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 63069U 26145.48315443 +.00000000 +00000-0 +44446-3 0 00002
2 63069 42.9991 73.4450 0001418 265.0684 95.0006 15.27590755 04
| Epoch (UTC): | 25 May 2026 11:35:44 |
| Eccentricity: | 0.0001418 |
| inclination: | 42.9991° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 73.4450° |
| argument of perigee: | 265.0684° |
| revolutions per day: | 15.27590755 |
| mean anomaly at epoch: | 95.0006° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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