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 26158.92461142 +.00000000 +00000-0 +51452-4 0 00004
2 02142 35.0472 20.8846 0007501 227.4868 132.5186 14.34694335 08
| Epoch (UTC): | 07 June 2026 22:11:26 |
| Eccentricity: | 0.0007501 |
| inclination: | 35.0472° |
| perigee height: | 771 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 20.8846° |
| argument of perigee: | 227.4868° |
| revolutions per day: | 14.34694335 |
| mean anomaly at epoch: | 132.5186° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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