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 57634U 26145.02970597 +.00000000 +00000-0 +69195-4 0 00009
2 57634 43.0043 10.2192 0001203 272.1489 87.9225 15.27582865 07
| Epoch (UTC): | 25 May 2026 00:42:46 |
| Eccentricity: | 0.0001203 |
| inclination: | 43.0043° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 10.2192° |
| argument of perigee: | 272.1489° |
| revolutions per day: | 15.27582865 |
| mean anomaly at epoch: | 87.9225° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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