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 63275U 26145.00274484 +.00000000 +00000-0 +15139-2 0 00004
2 63275 43.0016 12.0541 0001510 268.9103 91.1591 15.70877204 05
| Epoch (UTC): | 25 May 2026 00:03:57 |
| Eccentricity: | 0.0001510 |
| inclination: | 43.0016° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 12.0541° |
| argument of perigee: | 268.9103° |
| revolutions per day: | 15.70877204 |
| mean anomaly at epoch: | 91.1591° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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