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 63990U 26145.59751860 +.00000000 +00000-0 +72438-3 0 00006
2 63990 97.3631 221.4673 0008604 24.3425 335.8221 15.30477379 01
| Epoch (UTC): | 25 May 2026 14:20:25 |
| Eccentricity: | 0.0008604 |
| inclination: | 97.3631° |
| perigee height: | 468 km |
| apogee height: | 480 km |
| right ascension of ascending node: | 221.4673° |
| argument of perigee: | 24.3425° |
| revolutions per day: | 15.30477379 |
| mean anomaly at epoch: | 335.8221° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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