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 63641U 26144.83281992 +.00000000 +00000-0 +85792-3 0 00006
2 63641 43.0005 295.0544 0001877 269.1316 90.9321 15.27613856 02
| Epoch (UTC): | 24 May 2026 19:59:15 |
| Eccentricity: | 0.0001877 |
| inclination: | 43.0005° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 295.0544° |
| argument of perigee: | 269.1316° |
| revolutions per day: | 15.27613856 |
| mean anomaly at epoch: | 90.9321° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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