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 04071U 26073.59668058 +.00000000 +00000-0 +12418-3 0 00009
2 04071 74.0468 118.9866 0013968 348.4626 11.6221 14.66586224 09
| Epoch (UTC): | 14 March 2026 14:19:13 |
| Eccentricity: | 0.0013968 |
| inclination: | 74.0468° |
| perigee height: | 662 km |
| apogee height: | 682 km |
| right ascension of ascending node: | 118.9866° |
| argument of perigee: | 348.4626° |
| revolutions per day: | 14.66586224 |
| mean anomaly at epoch: | 11.6221° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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