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 26101.48646822 +.00000000 +00000-0 +15071-3 0 00000
2 00082 38.8637 247.5426 1167735 263.1522 83.5222 12.27890865 08
| Epoch (UTC): | 11 April 2026 11:40:30 |
| Eccentricity: | 0.1167735 |
| inclination: | 38.8637° |
| perigee height: | 632 km |
| apogee height: | 2485 km |
| right ascension of ascending node: | 247.5426° |
| argument of perigee: | 263.1522° |
| revolutions per day: | 12.27890865 |
| mean anomaly at epoch: | 83.5222° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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