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 02142U 26040.19348148 +.00000000 +00000-0 +73898-4 0 00001
2 02142 35.0465 309.9455 0006632 6.5626 353.5148 14.34663289 06
| Epoch (UTC): | 09 February 2026 04:38:36 |
| Eccentricity: | 0.0006632 |
| inclination: | 35.0465° |
| perigee height: | 771 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 309.9455° |
| argument of perigee: | 6.5626° |
| revolutions per day: | 14.34663289 |
| mean anomaly at epoch: | 353.5148° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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