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 26041.45478815 +.00000000 +00000-0 +87304-4 0 00006
2 23827 99.0399 61.5246 0002547 315.7328 44.3645 14.23691622 06
| Epoch (UTC): | 10 February 2026 10:54:53 |
| Eccentricity: | 0.0002547 |
| inclination: | 99.0399° |
| perigee height: | 811 km |
| apogee height: | 815 km |
| right ascension of ascending node: | 61.5246° |
| argument of perigee: | 315.7328° |
| revolutions per day: | 14.23691622 |
| mean anomaly at epoch: | 44.3645° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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