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 26039.14952362 +.00000000 +00000-0 +73078-4 0 00003
2 02142 35.0467 315.6519 0006725 358.3345 1.7320 14.34662832 09
| Epoch (UTC): | 08 February 2026 03:35:18 |
| Eccentricity: | 0.0006725 |
| inclination: | 35.0467° |
| perigee height: | 771 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 315.6519° |
| argument of perigee: | 358.3345° |
| revolutions per day: | 14.34662832 |
| mean anomaly at epoch: | 1.7320° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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