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 67805U 26145.49644233 +.00000000 +00000-0 +46927-3 0 00003
2 67805 97.2849 333.6184 0001643 90.0274 270.1157 15.33445282 01
| Epoch (UTC): | 25 May 2026 11:54:52 |
| Eccentricity: | 0.0001643 |
| inclination: | 97.2849° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 333.6184° |
| argument of perigee: | 90.0274° |
| revolutions per day: | 15.33445282 |
| mean anomaly at epoch: | 270.1157° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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