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 26037.58942677 +.00000000 +00000-0 +10238-3 0 00008
2 23827 99.0399 57.5533 0002719 329.3104 30.7914 14.23690128 02
| Epoch (UTC): | 06 February 2026 14:08:46 |
| Eccentricity: | 0.0002719 |
| inclination: | 99.0399° |
| perigee height: | 811 km |
| apogee height: | 815 km |
| right ascension of ascending node: | 57.5533° |
| argument of perigee: | 329.3104° |
| revolutions per day: | 14.23690128 |
| mean anomaly at epoch: | 30.7914° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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