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 63381U 26145.45610370 +.00000000 +00000-0 +78342-3 0 00005
2 63381 53.1573 55.8223 0001413 90.8809 269.2354 15.30205486 00
| Epoch (UTC): | 25 May 2026 10:56:47 |
| Eccentricity: | 0.0001413 |
| inclination: | 53.1573° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 55.8223° |
| argument of perigee: | 90.8809° |
| revolutions per day: | 15.30205486 |
| mean anomaly at epoch: | 269.2354° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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