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 63802U 26145.24358925 +.00000000 +00000-0 +81193-3 0 00003
2 63802 43.0003 339.8809 0001985 275.9264 84.1361 15.27592042 09
| Epoch (UTC): | 25 May 2026 05:50:46 |
| Eccentricity: | 0.0001985 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 339.8809° |
| argument of perigee: | 275.9264° |
| revolutions per day: | 15.27592042 |
| mean anomaly at epoch: | 84.1361° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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