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 23967U 26087.21017250 +.00000000 +00000-0 +00000-0 0 00001
2 23967 11.0397 17.5157 0003648 97.7057 114.4955 1.00239269 03
| Epoch (UTC): | 28 March 2026 05:02:38 |
| Eccentricity: | 0.0003648 |
| inclination: | 11.0397° |
| perigee height: | 35780 km |
| apogee height: | 35811 km |
| right ascension of ascending node: | 17.5157° |
| argument of perigee: | 97.7057° |
| revolutions per day: | 1.00239269 |
| mean anomaly at epoch: | 114.4955° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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