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 42805U 26145.07088191 +.00000000 +00000-0 +14343-4 0 00003
2 42805 86.3951 331.6312 0002030 87.7643 272.3786 14.34218743 04
| Epoch (UTC): | 25 May 2026 01:42:04 |
| Eccentricity: | 0.0002030 |
| inclination: | 86.3951° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 331.6312° |
| argument of perigee: | 87.7643° |
| revolutions per day: | 14.34218743 |
| mean anomaly at epoch: | 272.3786° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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