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 63466U 26145.56653647 +.00000000 +00000-0 +22657-3 0 00003
2 63466 42.9996 185.6549 0001588 268.0471 92.0199 15.27586950 02
| Epoch (UTC): | 25 May 2026 13:35:48 |
| Eccentricity: | 0.0001588 |
| inclination: | 42.9996° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 185.6549° |
| argument of perigee: | 268.0471° |
| revolutions per day: | 15.27586950 |
| mean anomaly at epoch: | 92.0199° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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