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 63119U 26145.42430946 +.00000000 +00000-0 +49988-3 0 00004
2 63119 42.9933 288.0558 0000802 39.1752 320.9158 15.27599782 08
| Epoch (UTC): | 25 May 2026 10:11:00 |
| Eccentricity: | 0.0000802 |
| inclination: | 42.9933° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 288.0558° |
| argument of perigee: | 39.1752° |
| revolutions per day: | 15.27599782 |
| mean anomaly at epoch: | 320.9158° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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