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 39237U 26106.80991836 +.00000000 +00000-0 +00000-0 0 00006
2 39237 0.0586 95.3400 0003165 281.7856 184.3905 1.00272847 09
| Epoch (UTC): | 16 April 2026 19:26:16 |
| Eccentricity: | 0.0003165 |
| inclination: | 0.0586° |
| perigee height: | 35773 km |
| apogee height: | 35800 km |
| right ascension of ascending node: | 95.3400° |
| argument of perigee: | 281.7856° |
| revolutions per day: | 1.00272847 |
| mean anomaly at epoch: | 184.3905° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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