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 53761U 26145.31084726 +.00000000 +00000-0 +46470-3 0 00008
2 53761 34.9779 96.5292 0006544 310.0226 49.9918 15.37609631 00
| Epoch (UTC): | 25 May 2026 07:27:37 |
| Eccentricity: | 0.0006544 |
| inclination: | 34.9779° |
| perigee height: | 449 km |
| apogee height: | 458 km |
| right ascension of ascending node: | 96.5292° |
| argument of perigee: | 310.0226° |
| revolutions per day: | 15.37609631 |
| mean anomaly at epoch: | 49.9918° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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