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 37791U 26145.63143705 +.00000000 +00000-0 +76243-4 0 00003
2 37791 98.0560 237.3736 0019163 263.8389 225.3641 14.68140624 06
| Epoch (UTC): | 25 May 2026 15:09:16 |
| Eccentricity: | 0.0019163 |
| inclination: | 98.0560° |
| perigee height: | 654 km |
| apogee height: | 681 km |
| right ascension of ascending node: | 237.3736° |
| argument of perigee: | 263.8389° |
| revolutions per day: | 14.68140624 |
| mean anomaly at epoch: | 225.3641° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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