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 63321U 26145.47712193 +.00000000 +00000-0 +48406-3 0 00005
2 63321 43.0000 316.9739 0001232 252.6241 107.4476 15.27599361 09
| Epoch (UTC): | 25 May 2026 11:27:03 |
| Eccentricity: | 0.0001232 |
| inclination: | 43.0000° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 316.9739° |
| argument of perigee: | 252.6241° |
| revolutions per day: | 15.27599361 |
| mean anomaly at epoch: | 107.4476° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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