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 26158.35368450 +.00000000 +00000-0 +17920-3 0 00001
2 00082 38.8585 36.3068 1166404 178.5061 181.9584 12.27912580 08
| Epoch (UTC): | 07 June 2026 08:29:18 |
| Eccentricity: | 0.1166404 |
| inclination: | 38.8585° |
| perigee height: | 633 km |
| apogee height: | 2484 km |
| right ascension of ascending node: | 36.3068° |
| argument of perigee: | 178.5061° |
| revolutions per day: | 12.27912580 |
| mean anomaly at epoch: | 181.9584° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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