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 23455U 26088.13233354 +.00000000 +00000-0 +66984-4 0 00007
2 23455 98.5054 61.4280 0008710 319.5569 40.4957 14.14659683 03
| Epoch (UTC): | 29 March 2026 03:10:33 |
| Eccentricity: | 0.0008710 |
| inclination: | 98.5054° |
| perigee height: | 837 km |
| apogee height: | 850 km |
| right ascension of ascending node: | 61.4280° |
| argument of perigee: | 319.5569° |
| revolutions per day: | 14.14659683 |
| mean anomaly at epoch: | 40.4957° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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