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 23712U 26145.28511088 +.00000000 +00000-0 +00000-0 0 00009
2 23712 14.0654 3.9246 0000889 88.8369 150.8027 1.00367187 04
| Epoch (UTC): | 25 May 2026 06:50:33 |
| Eccentricity: | 0.0000889 |
| inclination: | 14.0654° |
| perigee height: | 35756 km |
| apogee height: | 35764 km |
| right ascension of ascending node: | 3.9246° |
| argument of perigee: | 88.8369° |
| revolutions per day: | 1.00367187 |
| mean anomaly at epoch: | 150.8027° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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