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 62964U 26145.52244713 +.00000000 +00000-0 +38470-3 0 00001
2 62964 53.1582 233.2625 0001234 89.2347 270.8795 15.30194044 08
| Epoch (UTC): | 25 May 2026 12:32:19 |
| Eccentricity: | 0.0001234 |
| inclination: | 53.1582° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 233.2625° |
| argument of perigee: | 89.2347° |
| revolutions per day: | 15.30194044 |
| mean anomaly at epoch: | 270.8795° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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