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 63416U 26145.39833877 +.00000000 +00000-0 +10199-2 0 00001
2 63416 42.9995 33.6264 0002809 268.6492 91.4038 15.27614502 08
| Epoch (UTC): | 25 May 2026 09:33:36 |
| Eccentricity: | 0.0002809 |
| inclination: | 42.9995° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 33.6264° |
| argument of perigee: | 268.6492° |
| revolutions per day: | 15.27614502 |
| mean anomaly at epoch: | 91.4038° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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