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 23937U 26111.74721025 +.00000000 +00000-0 +20546-3 0 00006
2 23937 63.2433 215.5308 0016000 72.6256 287.6665 16.45774166 03
| Epoch (UTC): | 21 April 2026 17:55:58 |
| Eccentricity: | 0.0016000 |
| inclination: | 63.2433° |
| perigee height: | 140 km |
| apogee height: | 161 km |
| right ascension of ascending node: | 215.5308° |
| argument of perigee: | 72.6256° |
| revolutions per day: | 16.45774166 |
| mean anomaly at epoch: | 287.6665° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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