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 63769U 26145.49840176 +.00000000 +00000-0 +10249-2 0 00009
2 63769 43.0040 331.5307 0001756 275.0082 85.0569 15.27619016 00
| Epoch (UTC): | 25 May 2026 11:57:41 |
| Eccentricity: | 0.0001756 |
| inclination: | 43.0040° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 331.5307° |
| argument of perigee: | 275.0082° |
| revolutions per day: | 15.27619016 |
| mean anomaly at epoch: | 85.0569° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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