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 37384U 26148.76080692 +.00000000 +00000-0 +00000-0 0 00007
2 37384 62.3823 40.3343 0034407 185.4964 42.4945 1.00272941 07
| Epoch (UTC): | 28 May 2026 18:15:33 |
| Eccentricity: | 0.0034407 |
| inclination: | 62.3823° |
| perigee height: | 35641 km |
| apogee height: | 35931 km |
| right ascension of ascending node: | 40.3343° |
| argument of perigee: | 185.4964° |
| revolutions per day: | 1.00272941 |
| mean anomaly at epoch: | 42.4945° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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