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 42812U 26145.35337362 +.00000000 +00000-0 +70815-4 0 00005
2 42812 86.3986 3.2179 0002080 86.4930 273.6503 14.34219243 00
| Epoch (UTC): | 25 May 2026 08:28:51 |
| Eccentricity: | 0.0002080 |
| inclination: | 86.3986° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 3.2179° |
| argument of perigee: | 86.4930° |
| revolutions per day: | 14.34219243 |
| mean anomaly at epoch: | 273.6503° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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