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 26021.52612277 +.00000000 +00000-0 +13463-2 0 00001
2 37871 52.4556 230.8535 5753085 69.7825 341.3478 4.41915931 08
| Epoch (UTC): | 21 January 2026 12:37:37 |
| Eccentricity: | 0.5753085 |
| inclination: | 52.4556° |
| perigee height: | 284 km |
| apogee height: | 18332 km |
| right ascension of ascending node: | 230.8535° |
| argument of perigee: | 69.7825° |
| revolutions per day: | 4.41915931 |
| mean anomaly at epoch: | 341.3478° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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