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 26106.86695435 +.00000000 +00000-0 +30293-4 0 00004
2 02142 35.0465 305.4693 0006884 181.7940 178.2724 14.34683484 06
| Epoch (UTC): | 16 April 2026 20:48:24 |
| Eccentricity: | 0.0006884 |
| inclination: | 35.0465° |
| perigee height: | 771 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 305.4693° |
| argument of perigee: | 181.7940° |
| revolutions per day: | 14.34683484 |
| mean anomaly at epoch: | 178.2724° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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