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 63409U 26145.41505747 +.00000000 +00000-0 +66467-3 0 00008
2 63409 43.0031 33.8044 0002286 256.2998 103.7599 15.27593130 06
| Epoch (UTC): | 25 May 2026 09:57:40 |
| Eccentricity: | 0.0002286 |
| inclination: | 43.0031° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 33.8044° |
| argument of perigee: | 256.2998° |
| revolutions per day: | 15.27593130 |
| mean anomaly at epoch: | 103.7599° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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