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 67807U 26145.25445031 +.00000000 +00000-0 +39716-3 0 00002
2 67807 97.2865 333.3321 0001710 86.2497 273.8941 15.33454679 01
| Epoch (UTC): | 25 May 2026 06:06:24 |
| Eccentricity: | 0.0001710 |
| inclination: | 97.2865° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 333.3321° |
| argument of perigee: | 86.2497° |
| revolutions per day: | 15.33454679 |
| mean anomaly at epoch: | 273.8941° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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