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 11573U 26088.05976197 +.00000000 +00000-0 +60861-4 0 00003
2 11573 74.0670 213.6847 0016172 333.4662 26.5662 14.37598246 04
| Epoch (UTC): | 29 March 2026 01:26:03 |
| Eccentricity: | 0.0016172 |
| inclination: | 74.0670° |
| perigee height: | 755 km |
| apogee height: | 778 km |
| right ascension of ascending node: | 213.6847° |
| argument of perigee: | 333.4662° |
| revolutions per day: | 14.37598246 |
| mean anomaly at epoch: | 26.5662° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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