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 67540U 26145.42125872 +.00000000 +00000-0 +52870-3 0 00009
2 67540 97.2865 32.4752 0001787 93.9749 266.1698 15.33455900 01
| Epoch (UTC): | 25 May 2026 10:06:36 |
| Eccentricity: | 0.0001787 |
| inclination: | 97.2865° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 32.4752° |
| argument of perigee: | 93.9749° |
| revolutions per day: | 15.33455900 |
| mean anomaly at epoch: | 266.1698° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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