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 23787U 26104.12377160 +.00000000 +00000-0 +12070-3 0 00003
2 23787 82.5796 339.9302 0010882 183.2525 330.5068 12.64105440 02
| Epoch (UTC): | 14 April 2026 02:58:13 |
| Eccentricity: | 0.0010882 |
| inclination: | 82.5796° |
| perigee height: | 1398 km |
| apogee height: | 1415 km |
| right ascension of ascending node: | 339.9302° |
| argument of perigee: | 183.2525° |
| revolutions per day: | 12.64105440 |
| mean anomaly at epoch: | 330.5068° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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