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 26039.48696839 +.00000000 +00000-0 +92560-4 0 00004
2 23827 99.0399 59.5028 0002619 322.9313 37.1683 14.23690811 06
| Epoch (UTC): | 08 February 2026 11:41:14 |
| Eccentricity: | 0.0002619 |
| inclination: | 99.0399° |
| perigee height: | 811 km |
| apogee height: | 815 km |
| right ascension of ascending node: | 59.5028° |
| argument of perigee: | 322.9313° |
| revolutions per day: | 14.23690811 |
| mean anomaly at epoch: | 37.1683° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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