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 37187U 26069.54424934 +.00000000 +00000-0 +16277-2 0 00002
2 37187 49.5408 232.7592 5100245 139.3522 272.8840 5.40480741 04
| Epoch (UTC): | 10 March 2026 13:03:43 |
| Eccentricity: | 0.5100245 |
| inclination: | 49.5408° |
| perigee height: | 342 km |
| apogee height: | 14333 km |
| right ascension of ascending node: | 232.7592° |
| argument of perigee: | 139.3522° |
| revolutions per day: | 5.40480741 |
| mean anomaly at epoch: | 272.8840° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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