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 67580U 26145.44810963 +.00000000 +00000-0 +70610-3 0 00009
2 67580 97.2854 205.8676 0000469 102.8917 257.2378 15.33452969 05
| Epoch (UTC): | 25 May 2026 10:45:16 |
| Eccentricity: | 0.0000469 |
| inclination: | 97.2854° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 205.8676° |
| argument of perigee: | 102.8917° |
| revolutions per day: | 15.33452969 |
| mean anomaly at epoch: | 257.2378° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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