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 63480U 26145.55158995 +.00000000 +00000-0 +66171-3 0 00003
2 63480 43.0019 182.0557 0001846 257.6741 102.3904 15.27604443 04
| Epoch (UTC): | 25 May 2026 13:14:17 |
| Eccentricity: | 0.0001846 |
| inclination: | 43.0019° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 182.0557° |
| argument of perigee: | 257.6741° |
| revolutions per day: | 15.27604443 |
| mean anomaly at epoch: | 102.3904° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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