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 26140.38897310 +.00000000 +00000-0 +00000-0 0 00002
2 23967 11.0907 17.2363 0005451 100.9287 220.5563 1.00223557 09
| Epoch (UTC): | 20 May 2026 09:20:07 |
| Eccentricity: | 0.0005451 |
| inclination: | 11.0907° |
| perigee height: | 35777 km |
| apogee height: | 35823 km |
| right ascension of ascending node: | 17.2363° |
| argument of perigee: | 100.9287° |
| revolutions per day: | 1.00223557 |
| mean anomaly at epoch: | 220.5563° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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