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 07434U 26021.53238932 +.00000000 +00000-0 +11710-3 0 00000
2 07434 74.0439 203.1187 0019457 55.9039 304.3958 14.38156735 01
| Epoch (UTC): | 21 January 2026 12:46:38 |
| Eccentricity: | 0.0019457 |
| inclination: | 74.0439° |
| perigee height: | 751 km |
| apogee height: | 778 km |
| right ascension of ascending node: | 203.1187° |
| argument of perigee: | 55.9039° |
| revolutions per day: | 14.38156735 |
| mean anomaly at epoch: | 304.3958° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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