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 26073U 26088.19420911 +.00000000 +00000-0 +18108-3 0 00003
2 26073 71.0800 24.3728 0191758 67.6951 50.1692 13.74692763 08
| Epoch (UTC): | 29 March 2026 04:39:39 |
| Eccentricity: | 0.0191758 |
| inclination: | 71.0800° |
| perigee height: | 842 km |
| apogee height: | 1124 km |
| right ascension of ascending node: | 24.3728° |
| argument of perigee: | 67.6951° |
| revolutions per day: | 13.74692763 |
| mean anomaly at epoch: | 50.1692° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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