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 26068.34889432 +.00000000 +00000-0 +70796-4 0 00007
2 14148 82.5212 161.6525 0019235 257.1881 102.7186 14.85668209 02
| Epoch (UTC): | 09 March 2026 08:22:24 |
| Eccentricity: | 0.0019235 |
| inclination: | 82.5212° |
| perigee height: | 598 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 161.6525° |
| argument of perigee: | 257.1881° |
| revolutions per day: | 14.85668209 |
| mean anomaly at epoch: | 102.7186° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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