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 63789U 26145.51541508 +.00000000 +00000-0 +46637-3 0 00002
2 63789 43.0015 338.4874 0001168 280.9262 79.1458 15.27593979 01
| Epoch (UTC): | 25 May 2026 12:22:11 |
| Eccentricity: | 0.0001168 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 338.4874° |
| argument of perigee: | 280.9262° |
| revolutions per day: | 15.27593979 |
| mean anomaly at epoch: | 79.1458° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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