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 67756U 26145.11454498 +.00000000 +00000-0 +00000-0 0 00008
2 67756 0.2968 303.9151 0001430 182.4372 233.6584 1.00271356 01
| Epoch (UTC): | 25 May 2026 02:44:56 |
| Eccentricity: | 0.0001430 |
| inclination: | 0.2968° |
| perigee height: | 35781 km |
| apogee height: | 35793 km |
| right ascension of ascending node: | 303.9151° |
| argument of perigee: | 182.4372° |
| revolutions per day: | 1.00271356 |
| mean anomaly at epoch: | 233.6584° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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