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 37871U 26021.97864639 +.00000000 +00000-0 +14799-2 0 00004
2 37871 52.4554 230.5891 5753013 69.9667 341.2767 4.41924425 03
| Epoch (UTC): | 21 January 2026 23:29:15 |
| Eccentricity: | 0.5753013 |
| inclination: | 52.4554° |
| perigee height: | 284 km |
| apogee height: | 18332 km |
| right ascension of ascending node: | 230.5891° |
| argument of perigee: | 69.9667° |
| revolutions per day: | 4.41924425 |
| mean anomaly at epoch: | 341.2767° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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