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 42836U 26150.40428196 +.00000000 +00000-0 +42690-3 0 00008
2 42836 97.4233 312.9609 0004900 144.5945 215.5610 15.08759816 08
| Epoch (UTC): | 30 May 2026 09:42:09 |
| Eccentricity: | 0.0004900 |
| inclination: | 97.4233° |
| perigee height: | 537 km |
| apogee height: | 543 km |
| right ascension of ascending node: | 312.9609° |
| argument of perigee: | 144.5945° |
| revolutions per day: | 15.08759816 |
| mean anomaly at epoch: | 215.5610° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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