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 63289U 26145.49482067 +.00000000 +00000-0 +23692-3 0 00004
2 63289 82.4913 92.6696 0022283 72.7492 287.6024 12.42876451 02
| Epoch (UTC): | 25 May 2026 11:52:32 |
| Eccentricity: | 0.0022283 |
| inclination: | 82.4913° |
| perigee height: | 1477 km |
| apogee height: | 1512 km |
| right ascension of ascending node: | 92.6696° |
| argument of perigee: | 72.7492° |
| revolutions per day: | 12.42876451 |
| mean anomaly at epoch: | 287.6024° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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