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 37849U 26145.57350528 +.00000000 +00000-0 +51888-4 0 00001
2 37849 98.7947 86.6052 0002578 52.1763 307.9646 14.19512010 09
| Epoch (UTC): | 25 May 2026 13:45:50 |
| Eccentricity: | 0.0002578 |
| inclination: | 98.7947° |
| perigee height: | 825 km |
| apogee height: | 829 km |
| right ascension of ascending node: | 86.6052° |
| argument of perigee: | 52.1763° |
| revolutions per day: | 14.19512010 |
| mean anomaly at epoch: | 307.9646° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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