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 23094U 26087.73846925 +.00000000 +00000-0 +14047-3 0 00007
2 23094 70.9870 195.6344 0198463 119.5103 352.8434 13.74371096 04
| Epoch (UTC): | 28 March 2026 17:43:23 |
| Eccentricity: | 0.0198463 |
| inclination: | 70.9870° |
| perigee height: | 838 km |
| apogee height: | 1130 km |
| right ascension of ascending node: | 195.6344° |
| argument of perigee: | 119.5103° |
| revolutions per day: | 13.74371096 |
| mean anomaly at epoch: | 352.8434° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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