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 67835U 26145.49633875 +.00000000 +00000-0 +61798-3 0 00009
2 67835 42.9993 193.0161 0001487 268.5703 91.4978 15.27571128 06
| Epoch (UTC): | 25 May 2026 11:54:43 |
| Eccentricity: | 0.0001487 |
| inclination: | 42.9993° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 193.0161° |
| argument of perigee: | 268.5703° |
| revolutions per day: | 15.27571128 |
| mean anomaly at epoch: | 91.4978° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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