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 63067U 26145.49472043 +.00000000 +00000-0 +68353-3 0 00004
2 63067 42.9992 73.5287 0001714 280.7152 79.3507 15.27589760 00
| Epoch (UTC): | 25 May 2026 11:52:23 |
| Eccentricity: | 0.0001714 |
| inclination: | 42.9992° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 73.5287° |
| argument of perigee: | 280.7152° |
| revolutions per day: | 15.27589760 |
| mean anomaly at epoch: | 79.3507° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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