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 63045U 26145.35296963 +.00000000 +00000-0 +57133-3 0 00004
2 63045 53.1605 274.8602 0001185 74.3393 285.7739 15.30214386 07
| Epoch (UTC): | 25 May 2026 08:28:16 |
| Eccentricity: | 0.0001185 |
| inclination: | 53.1605° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 274.8602° |
| argument of perigee: | 74.3393° |
| revolutions per day: | 15.30214386 |
| mean anomaly at epoch: | 285.7739° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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