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 26073.83234297 +.00000000 +00000-0 +21757-3 0 00004
2 00082 38.8579 350.2588 1166615 129.2893 241.7227 12.27875297 08
| Epoch (UTC): | 14 March 2026 19:58:34 |
| Eccentricity: | 0.1166615 |
| inclination: | 38.8579° |
| perigee height: | 633 km |
| apogee height: | 2484 km |
| right ascension of ascending node: | 350.2588° |
| argument of perigee: | 129.2893° |
| revolutions per day: | 12.27875297 |
| mean anomaly at epoch: | 241.7227° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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