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 37809U 26145.56648169 +.00000000 +00000-0 +00000-0 0 00003
2 37809 0.0206 68.2589 0003001 358.3993 293.4315 1.00268421 00
| Epoch (UTC): | 25 May 2026 13:35:44 |
| Eccentricity: | 0.0003001 |
| inclination: | 0.0206° |
| perigee height: | 35775 km |
| apogee height: | 35800 km |
| right ascension of ascending node: | 68.2589° |
| argument of perigee: | 358.3993° |
| revolutions per day: | 1.00268421 |
| mean anomaly at epoch: | 293.4315° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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