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 26039.55724772 +.00000000 +00000-0 +89515-4 0 00006
2 23827 99.0399 59.5750 0002615 322.7100 37.3896 14.23690796 06
| Epoch (UTC): | 08 February 2026 13:22:26 |
| Eccentricity: | 0.0002615 |
| inclination: | 99.0399° |
| perigee height: | 811 km |
| apogee height: | 815 km |
| right ascension of ascending node: | 59.5750° |
| argument of perigee: | 322.7100° |
| revolutions per day: | 14.23690796 |
| mean anomaly at epoch: | 37.3896° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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