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 63991U 26145.61354191 +.00000000 +00000-0 +64804-3 0 00004
2 63991 97.3640 218.9219 0011896 52.7959 307.4360 15.19862746 05
| Epoch (UTC): | 25 May 2026 14:43:30 |
| Eccentricity: | 0.0011896 |
| inclination: | 97.3640° |
| perigee height: | 498 km |
| apogee height: | 514 km |
| right ascension of ascending node: | 218.9219° |
| argument of perigee: | 52.7959° |
| revolutions per day: | 15.19862746 |
| mean anomaly at epoch: | 307.4360° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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