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 26041.94674291 +.00000000 +00000-0 +86132-4 0 00004
2 23827 99.0398 62.0300 0002533 313.8902 46.2066 14.23691808 08
| Epoch (UTC): | 10 February 2026 22:43:18 |
| Eccentricity: | 0.0002533 |
| inclination: | 99.0398° |
| perigee height: | 811 km |
| apogee height: | 815 km |
| right ascension of ascending node: | 62.0300° |
| argument of perigee: | 313.8902° |
| revolutions per day: | 14.23691808 |
| mean anomaly at epoch: | 46.2066° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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