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 26065.52012980 +.00000000 +00000-0 +79930-4 0 00009
2 14148 82.5212 164.3109 0019230 267.3225 92.5790 14.85664567 00
| Epoch (UTC): | 06 March 2026 12:28:59 |
| Eccentricity: | 0.0019230 |
| inclination: | 82.5212° |
| perigee height: | 598 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 164.3109° |
| argument of perigee: | 267.3225° |
| revolutions per day: | 14.85664567 |
| mean anomaly at epoch: | 92.5790° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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