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 26053.76489218 +.00000000 +00000-0 +45673-4 0 00002
2 02142 35.0441 235.7565 0006189 121.7365 238.3927 14.34667369 03
| Epoch (UTC): | 22 February 2026 18:21:26 |
| Eccentricity: | 0.0006189 |
| inclination: | 35.0441° |
| perigee height: | 772 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 235.7565° |
| argument of perigee: | 121.7365° |
| revolutions per day: | 14.34667369 |
| mean anomaly at epoch: | 238.3927° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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