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 63688U 26145.59444782 +.00000000 +00000-0 +14619-3 0 00009
2 63688 86.5062 320.7983 0001496 78.0314 282.0988 13.24407707 07
| Epoch (UTC): | 25 May 2026 14:16:00 |
| Eccentricity: | 0.0001496 |
| inclination: | 86.5062° |
| perigee height: | 1167 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 320.7983° |
| argument of perigee: | 78.0314° |
| revolutions per day: | 13.24407707 |
| mean anomaly at epoch: | 282.0988° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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