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 67535U 26145.41581306 +.00000000 +00000-0 +27146-3 0 00008
2 67535 97.2867 32.4849 0001460 101.2358 258.9049 15.33439929 03
| Epoch (UTC): | 25 May 2026 09:58:46 |
| Eccentricity: | 0.0001460 |
| inclination: | 97.2867° |
| perigee height: | 465 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 32.4849° |
| argument of perigee: | 101.2358° |
| revolutions per day: | 15.33439929 |
| mean anomaly at epoch: | 258.9049° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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