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 14148U 26159.47307295 +.00000000 +00000-0 +48372-4 0 00009
2 14148 82.5184 75.9633 0019671 320.3462 39.6315 14.85742975 04
| Epoch (UTC): | 08 June 2026 11:21:13 |
| Eccentricity: | 0.0019671 |
| inclination: | 82.5184° |
| perigee height: | 598 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 75.9633° |
| argument of perigee: | 320.3462° |
| revolutions per day: | 14.85742975 |
| mean anomaly at epoch: | 39.6315° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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