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 63684U 26145.51814473 +.00000000 +00000-0 +68455-3 0 00002
2 63684 43.0021 316.6992 0001155 273.9926 86.0794 15.27593201 04
| Epoch (UTC): | 25 May 2026 12:26:07 |
| Eccentricity: | 0.0001155 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 316.6992° |
| argument of perigee: | 273.9926° |
| revolutions per day: | 15.27593201 |
| mean anomaly at epoch: | 86.0794° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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