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 00082U 26087.90279850 +.00000000 +00000-0 +22619-3 0 00009
2 00082 38.8588 297.9933 1167082 197.4337 158.2806 12.27883168 09
| Epoch (UTC): | 28 March 2026 21:40:01 |
| Eccentricity: | 0.1167082 |
| inclination: | 38.8588° |
| perigee height: | 632 km |
| apogee height: | 2485 km |
| right ascension of ascending node: | 297.9933° |
| argument of perigee: | 197.4337° |
| revolutions per day: | 12.27883168 |
| mean anomaly at epoch: | 158.2806° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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