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 23439U 26088.20712185 +.00000000 +00000-0 -28115-3 0 00005
2 23439 64.8147 72.5638 0153406 18.3966 342.2423 11.27583746 00
| Epoch (UTC): | 29 March 2026 04:58:15 |
| Eccentricity: | 0.0153406 |
| inclination: | 64.8147° |
| perigee height: | 1893 km |
| apogee height: | 2151 km |
| right ascension of ascending node: | 72.5638° |
| argument of perigee: | 18.3966° |
| revolutions per day: | 11.27583746 |
| mean anomaly at epoch: | 342.2423° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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