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 63589U 26145.62298266 +.00000000 +00000-0 +78645-3 0 00006
2 63589 42.9996 247.4501 0001522 271.9260 88.1417 15.27602040 08
| Epoch (UTC): | 25 May 2026 14:57:05 |
| Eccentricity: | 0.0001522 |
| inclination: | 42.9996° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 247.4501° |
| argument of perigee: | 271.9260° |
| revolutions per day: | 15.27602040 |
| mean anomaly at epoch: | 88.1417° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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