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 63421U 26145.40862760 +.00000000 +00000-0 +80445-3 0 00004
2 63421 43.0025 33.7012 0001111 268.5380 91.5344 15.27591239 04
| Epoch (UTC): | 25 May 2026 09:48:25 |
| Eccentricity: | 0.0001111 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 33.7012° |
| argument of perigee: | 268.5380° |
| revolutions per day: | 15.27591239 |
| mean anomaly at epoch: | 91.5344° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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