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 23090U 26088.00441738 +.00000000 +00000-0 +10729-3 0 00000
2 23090 71.0326 193.6886 0191192 356.7195 3.2638 13.75653897 01
| Epoch (UTC): | 29 March 2026 00:06:21 |
| Eccentricity: | 0.0191192 |
| inclination: | 71.0326° |
| perigee height: | 839 km |
| apogee height: | 1120 km |
| right ascension of ascending node: | 193.6886° |
| argument of perigee: | 356.7195° |
| revolutions per day: | 13.75653897 |
| mean anomaly at epoch: | 3.2638° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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