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 67660U 26145.35917227 +.00000000 +00000-0 +56184-3 0 00009
2 67660 97.2849 178.6288 0001029 172.1354 187.9905 15.33446875 06
| Epoch (UTC): | 25 May 2026 08:37:12 |
| Eccentricity: | 0.0001029 |
| inclination: | 97.2849° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 178.6288° |
| argument of perigee: | 172.1354° |
| revolutions per day: | 15.33446875 |
| mean anomaly at epoch: | 187.9905° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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