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 67574U 26145.13270963 +.00000000 +00000-0 +36434-3 0 00004
2 67574 97.2853 205.5319 0000265 342.4735 17.6498 15.33448269 01
| Epoch (UTC): | 25 May 2026 03:11:06 |
| Eccentricity: | 0.0000265 |
| inclination: | 97.2853° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 205.5319° |
| argument of perigee: | 342.4735° |
| revolutions per day: | 15.33448269 |
| mean anomaly at epoch: | 17.6498° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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