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 63602U 26145.59040904 +.00000000 +00000-0 +45314-4 0 00000
2 63602 99.6929 153.1654 0001189 90.0917 270.0357 13.57246728 02
| Epoch (UTC): | 25 May 2026 14:10:11 |
| Eccentricity: | 0.0001189 |
| inclination: | 99.6929° |
| perigee height: | 1045 km |
| apogee height: | 1047 km |
| right ascension of ascending node: | 153.1654° |
| argument of perigee: | 90.0917° |
| revolutions per day: | 13.57246728 |
| mean anomaly at epoch: | 270.0357° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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