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 23547U 26088.20053536 +.00000000 +00000-0 +37698-3 0 00008
2 23547 69.9759 57.1019 0006193 83.4178 276.7669 14.67247225 04
| Epoch (UTC): | 29 March 2026 04:48:46 |
| Eccentricity: | 0.0006193 |
| inclination: | 69.9759° |
| perigee height: | 666 km |
| apogee height: | 674 km |
| right ascension of ascending node: | 57.1019° |
| argument of perigee: | 83.4178° |
| revolutions per day: | 14.67247225 |
| mean anomaly at epoch: | 276.7669° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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