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 26146.26383578 +.00000000 +00000-0 +00000-0 0 00009
2 23712 14.0657 3.9170 0000991 90.7262 142.5599 1.00367289 06
| Epoch (UTC): | 26 May 2026 06:19:55 |
| Eccentricity: | 0.0000991 |
| inclination: | 14.0657° |
| perigee height: | 35756 km |
| apogee height: | 35764 km |
| right ascension of ascending node: | 3.9170° |
| argument of perigee: | 90.7262° |
| revolutions per day: | 1.00367289 |
| mean anomaly at epoch: | 142.5599° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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