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 63703U 26145.58985106 +.00000000 +00000-0 +34715-3 0 00005
2 63703 53.1590 222.3403 0000796 92.0337 268.0755 15.30204561 06
| Epoch (UTC): | 25 May 2026 14:09:23 |
| Eccentricity: | 0.0000796 |
| inclination: | 53.1590° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 222.3403° |
| argument of perigee: | 92.0337° |
| revolutions per day: | 15.30204561 |
| mean anomaly at epoch: | 268.0755° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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