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 23827U 26039.06529258 +.00000000 +00000-0 +90302-4 0 00000
2 23827 99.0399 59.0696 0002642 324.3854 35.7147 14.23690596 03
| Epoch (UTC): | 08 February 2026 01:34:01 |
| Eccentricity: | 0.0002642 |
| inclination: | 99.0399° |
| perigee height: | 811 km |
| apogee height: | 815 km |
| right ascension of ascending node: | 59.0696° |
| argument of perigee: | 324.3854° |
| revolutions per day: | 14.23690596 |
| mean anomaly at epoch: | 35.7147° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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