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 42967U 26145.56292832 +.00000000 +00000-0 +00000-0 0 00006
2 42967 0.0215 11.5104 0002785 46.2873 283.0544 1.00271622 09
| Epoch (UTC): | 25 May 2026 13:30:37 |
| Eccentricity: | 0.0002785 |
| inclination: | 0.0215° |
| perigee height: | 35775 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 11.5104° |
| argument of perigee: | 46.2873° |
| revolutions per day: | 1.00271622 |
| mean anomaly at epoch: | 283.0544° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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