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 26071.55026720 +.00000000 +00000-0 +13146-3 0 00006
2 04071 74.0474 122.9299 0013874 352.7681 7.3286 14.66583431 06
| Epoch (UTC): | 12 March 2026 13:12:23 |
| Eccentricity: | 0.0013874 |
| inclination: | 74.0474° |
| perigee height: | 662 km |
| apogee height: | 682 km |
| right ascension of ascending node: | 122.9299° |
| argument of perigee: | 352.7681° |
| revolutions per day: | 14.66583431 |
| mean anomaly at epoch: | 7.3286° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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