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 63090U 26145.44271676 +.00000000 +00000-0 +33010-3 0 00006
2 63090 70.0002 160.7475 0003976 263.8555 96.2151 14.98336498 07
| Epoch (UTC): | 25 May 2026 10:37:30 |
| Eccentricity: | 0.0003976 |
| inclination: | 70.0002° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 160.7475° |
| argument of perigee: | 263.8555° |
| revolutions per day: | 14.98336498 |
| mean anomaly at epoch: | 96.2151° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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