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 63280U 26145.43801134 +.00000000 +00000-0 +34355-3 0 00007
2 63280 43.0008 168.1252 0001521 262.9968 97.0710 15.27583162 06
| Epoch (UTC): | 25 May 2026 10:30:44 |
| Eccentricity: | 0.0001521 |
| inclination: | 43.0008° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 168.1252° |
| argument of perigee: | 262.9968° |
| revolutions per day: | 15.27583162 |
| mean anomaly at epoch: | 97.0710° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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