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 26088.21518705 +.00000000 +00000-0 +49821-4 0 00003
2 02142 35.0466 47.4282 0006530 25.0959 335.0045 14.34677931 01
| Epoch (UTC): | 29 March 2026 05:09:52 |
| Eccentricity: | 0.0006530 |
| inclination: | 35.0466° |
| perigee height: | 771 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 47.4282° |
| argument of perigee: | 25.0959° |
| revolutions per day: | 14.34677931 |
| mean anomaly at epoch: | 335.0045° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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