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 42807U 26145.08063582 +.00000000 +00000-0 +85441-5 0 00001
2 42807 86.3985 3.2957 0002233 86.7802 273.3649 14.34217856 04
| Epoch (UTC): | 25 May 2026 01:56:06 |
| Eccentricity: | 0.0002233 |
| inclination: | 86.3985° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 3.2957° |
| argument of perigee: | 86.7802° |
| revolutions per day: | 14.34217856 |
| mean anomaly at epoch: | 273.3649° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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