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 63988U 26145.63830007 +.00000000 +00000-0 +17567-3 0 00001
2 63988 97.3702 220.9379 0013398 32.4532 327.7528 15.26425233 06
| Epoch (UTC): | 25 May 2026 15:19:09 |
| Eccentricity: | 0.0013398 |
| inclination: | 97.3702° |
| perigee height: | 477 km |
| apogee height: | 496 km |
| right ascension of ascending node: | 220.9379° |
| argument of perigee: | 32.4532° |
| revolutions per day: | 15.26425233 |
| mean anomaly at epoch: | 327.7528° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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