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 26071.67475328 +.00000000 +00000-0 +96345-4 0 00004
2 23827 99.0377 92.5722 0002892 199.9282 160.1783 14.23703916 09
| Epoch (UTC): | 12 March 2026 16:11:38 |
| Eccentricity: | 0.0002892 |
| inclination: | 99.0377° |
| perigee height: | 811 km |
| apogee height: | 815 km |
| right ascension of ascending node: | 92.5722° |
| argument of perigee: | 199.9282° |
| revolutions per day: | 14.23703916 |
| mean anomaly at epoch: | 160.1783° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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